Analysis of Turbulent Flows with Computer Programs

Analysis of Turbulent Flows with Computer Programs

Volumn , Issue , 2004, Pages 1-376

  Cebeci, Tuncer ^a  

^a BOEING COMPANY   (United States)

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References (303)

1. L. Prandtl (1926) Turbulent flow. 2nd Int. Congr. Appl. Mech. Zurich NACA Tech. Memo, 435, originally delivered to
2. Tennekes, H. and Lumley, J. L.: A First Course in Turbulence, MIT Press, Cambridge, MA.
3. M. Lesieur (1994) La Turbulence. Press Universitaires de Grenoble
4. S.B. Pope (2000) Turbulent Flows. Cambridge Univ. Press
5. P.A. Durbin and B.A. Petterson (2001) Statistical Theory and Modeling of Turbulent Flows. John Wiley and Sons
6. W.C. Wilcox (1998) Turbulence Modeling for CFD. New York: DCW Industries
7. T. von Kármán (1937) Turbulence. Twenty-fifth Wilbur Wright Memorial Lecture. J. Roy. Aeronaut. Soc. 41 1109.
8. J.O. Hinze (1959) Turbulence, an Introduction to Its Mechanism and Theory. La Canada, CA: McGraw-Hill
9. G. Hagen (1839) On the motion of water in narrow cylindrical tubes (German). Pogg. Ann. 46 423.
10. L. Prandtl and O.G. Tietjens (1934) Applied Hydro- and Aeromechanics. New York: Dover 29.
11. O. Reynolds (1883) An experimental investigation of the circumstances which determine whether the motion of water will be direct or sinuous and the law of resistance in parallel channels. Phil. Trans. Roy. Soc. London 174 935.
12. J.H. Preston (1957) The minimum Reynolds number for a turbulent boundary layer and selection of a transition device. J. Fluid Mech. 3 373.
13. C.S. Wells (1967) Effects of free-stream turbulence on boundary-layer transition. AIAA J. 5 172.
14. A.M. Kolmogorov (1942) Equations of turbulent motion of an incompressible fluid. Izvestia Academy of Sciences, USSR; Physics vol. 6 56-58. nos. 1 and 2
15. A.M.O. Smith and D.W. Clutter (1957) The smallest height of roughness capable of affecting boundary-layer transition in low-speed flow. Douglas Aircraft Co. Rep. ES 26803 Ad 149 907
16. G.K. Batchelor (1953) The Theory of Homogeneous Turbulence. New York: Cambridge Univ. Press
17. P.S. Klebanoff (1954) Characteristics of turbulence in a boundary layer with zero pressure gradient. NACA Tech. Note 3178
18. H. Eckelmann (1970) Experimentelle Untersuchungen in einer turbulenten Kanalströmung mit starken viskosen Wandschichten. Mitt. No. 48, Max-Planck-Inst. for Flow Res., Göttingen
19. G.B. Schubauer and P.S. Klebanoff (1950) Investigation of separation of the turbulent boundary layer. NACA Tech. Note No. 2133
20. G.K. Batchelor and A.A. Townsend (1948) Decay of turbulence in the final period. Proc. Roy Soc. 194A 527.
21. A. Favre, J. Gaviglio and R. Dumas (1953) Quelques mesures de correlation dans le temps et l'espace en soufflerie. Rech. Aeronaut 32 21.
22. H.W. Liepmann (1952) On the application of statistical concepts to the buffeting problem. J. Aeronaut Sci. 19 793.
23. G.K. Batchelor (1967) An Introduction to Fluid Dynamics. London New York: Cambridge Univ. Press
24. S. Corrsin and A.L. Kistler (1954) The free-stream boundaries of turbulent flows. NACA Tech. Note No. 3133
25. O.M. Phillips (1955) The irrotational motion outside a free turbulent boundary layer. Proc. Camb. Phil. Soc. 51 220.
26. G.I. Taylor (1921) Diffusion by continuous movements. Proc. London Math. Soc. 20 196.
27. J. Samgorinsky (1963) General Circulation Experiments with the Primitive Equations. I. The Basic Experiment. Monthly Weather Review 91 99.
28. M. Germano, U. Piomelli, P. Moin and W.H. Cabot (1991) A Dynamic Subgrid-Scale Eddy-Viscosity Model. Phys. Fluids A3 1760.
29. N.N. Mansour, J. Kim and P. Moin (1988) Reynolds-Stress and Dissipation-Rate Budgets in a Turbulent Channel Flow. J. Fluid Mech. 194 15.
30. R.S. Rogallo (1981) Numerical Experiments in Homogeneous Turbulence. NASA TM 81315
31. J. Kim and P. Moin (1985) Application of a Fractional Step Method to Incompressible Navier-Stokes Equation. J. Comp. Phys. 59 308. and NASA TM85898, N84-22328, 1985
32. M.M. Rai and P. Moin (1991) Direct Simulations of Turbulent Flow Using Finite-Difference Schemes. J. Comp. Phys. 96 15.
33. L.H. Back (1970) Conservation equations of a viscous, heat-conducting fluid in curvilinear orthogonal coordinates. R.E. Boze, G.L. Tuve (Eds) Handbook of Tables for Applied Engineering Science London New York: Chem. Rubber Co. 415. Published in
34. H.W. Liepmann and A. Roshko (1952) Elements of Gas Dynamics. Cleveland, Ohio: Wiley 332.
35. P. Bradshaw (1971) An Introduction to Turbulence and Its Measurement. New York: Pergamon
36. E.R. Van Driest (1951) Turbulent Boundary Layer in Compressible Fluids. J. Aeronaut. Sci. 18 145.
37. A. Favre (1969) Statistical equations of turbulent gases. (part I) J. Mec. 4 361. SIAM Problems of Hydrodynamics and Continuum Mechanics (Sedov 60th birthday volume). Also, Equations des gaz turbulents compressibles
38. A. Favre (1969) Statistical equations of turbulent gases. (part II) J. Mec. 4 391. SIAM Problems of Hydrodynamics and Continuum Mechanics (Sedov 60th birthday volume). Also, Equations des gaz turbulents compressibles
39. J. Laufer and K.G. Ludloff (1970) Conservation equations in a compressible turbulent fluid and a numerical scheme for their solution. McDonnell Douglas Paper WD 1355
40. T. Cebeci and J. Cousteix (1998) Modeling and Computation of Boundary-Layer Flows. Oxford: Horizons Publ., Long Beach and Springer-Verlag
41. A.L. Kistler (1959) Fluctuation measurements in a supersonic turbulent boundary layer. Phys. Fluids 2 290.
42. M.V. Morkovin and W.S. Chen (1961) Effects of compressibility on turbulent flows. The Mechanics of Turbulence Berlin: Gordon and Breach 367.
43. A. Demetriades (1968) Turbulence measurements in an axisymmetric compressible wake. Phys. Fluids 11 1841.
44. A.L. Kistler and W.S. Chen (1963) The fluctuating pressure field in a supersonic turbulent boundary layer. J. Fluid Mech. 16 41.
45. J. Laufer (1964) Some statistical properties of the pressure field radiated by a turbulent boundary layer. Phys. Fluids 7 1191.
46. P.S. Klebanoff and Z.W. Diehl (1952) Some features of artificially thickened fully developed turbulent boundary layers with zero pressure gradient. NACA Rep. 1110
47. W. Jacobs (1939) Umformung eines turbulenten Geschwindigkeitsprofils. Z. Angew. Math. Mech. 19 87.
48. P.H. Hoffmann and A.E. Perry (1979) The development of turbulent thermal layers on flat plates. Int. J. Heat Mass Transfer 22 39.
49. T. van Kármán (1931) Mechanical similitude and turbulence. NACA Tech. Memo No. 611
50. P.S. Klebanoff (1954) Characteristics of turbulence in a boundary layer with zero pressure gradient. NACA Tech. Note 3178
51. D. Coles (1978) A Model for Flow in the Viscous Sublayer. Proceedings of the Workshop on Coherent Structure of Turbulent Boundary Layers New York: Lehigh University
52. M.M.M. El Telbany and A.J. Reynolds (1981) Turbulence in Plane Channel flows. Journal of Fiuid Mechanics 111 283-318.
53. V.C. Patel, W. Rodi and G. Scheuerer (1985) Turbulence models for near-wall and low Reynolds number flows: A Review. AIAA J. 23(No. 9), 1308-1319.
54. J.C. Rotta (1962) Turbulent Boundary Layers in Incompressible Flow. Progress in the Aeronautical Sciences 2 1-219.
55. B.E. Launder (1982) Second Moment Closure: Methodology and Practice. Proceedings of the Ecole d'Eté d'Analyse Numerique — Modelisation Numerique de la Turbulence Clamart, France
56. H.-P. Kreplin and H. Eckelmann (1979) Behaviour of the Three Fluctuating Velocity Components in the Wall Region of a Turbulent Channel Flow. Physics of Fluids 22 1233-1239.
57. K.K. Sirkar and T.J. Hanratty (1970) The Limiting Behaviour of the Turbulent Transverse Velocity Component Close to a Wall. J. Fluid Mech. 44 605-614.
58. R.W. Derksen and R.S. Azad (1981) Behaviour of the Turbulent Energy Equation at a Fixed Boundary. AIAA J. 19 238-239.
59. L. Laufer (1954) The Structure of Turbulence in Fully Developed Pipe Flow. NACA Rept. 1174
60. J. Boussinesq (1877) Theorie de l'écoulement tourbillant. Mem. Pres. Acad. Sci. XXIII 46 Paris
61. L. Prandtl (1926) Turbulent flow. 2nd Internat. Congr. Appl. Mech. Zürich NACA Tech. Memo, 435. Originally delivered to
62. W.P. Jones and B.E. Launder (1972) The prediction of laminarization with a two-equation model of turbulence. Int. J. Heat Mass Transfer 15 301.
63. S. Corrsin and A.L. Kistler (1954) The free-stream boundaries of turbulent flows. NACA Tech. Note No. 3133
64. J. Nikuradse (1955) Law of flow in rough pipes. Tech. Memo. NACA No. 1292
65. W. Nunner (1956) Wärmeübertragung und Druckabfall in rauhen Rohren. VDI-Forschungsheft No. 455
66. G.B. Schubauer (1954) Turbulent processes as observed in boundary layer and pipe. J. Appl. Phys. 25 188.
67. E.R. Van Driest (1956) On turbulent flow near a wall. J. Aeronaut. Sci. 23
68. K. Wieghardt (1944) Zum Reibungswiderstand rauher Platten. Bethlehem, Pa.: Kaiser-Wilhelm-Institut für Strömungsforschung UM 6612
69. T. Cebeci (1973) A model for eddy conductivity and turbulent Prandtl number. J. Heat Transfer 95 227.
70. F.H. Clauser (1956) The turbulent boundary layer. Advan. Appl. Mech. 4 1.
71. D.W. Smith and J.H. Walker (1959) Skin friction measurements in incompressible flow. NASA Tech. Rep. R-26
72. F.H. Clauser (1954) Turbulent boundary layers in adverse pressure gradient. J. Aero. Sci. 21 91.
73. P. Bradshaw (1967) The turbulence structure of equilibrium boundary layers. NPL Aero. Rep. 1184
74. T.F. Herring and J. Norbury (1967) Some experiments on equilibrium turbulent boundary layers in favorable pressure gradients. J. Fluid Mech. 27 541.
75. D. Coles (1956) The law of the wake in the turbulent boundary layer. J. Fluid Mech. 1 191.
76. P.S. Granville (1976) A modified law of the wake for turbulent shear layers. J. Fluids Engineering 578-579. Sept.
77. B.G.J. Thompson (1965) A Near Two-parameter Family of Mean Velocity Profiles for Incompressible Boundary layers on Smooth Walls. ARC R&M 3463.
78. V.A. Ioselevich and V.I. Pilipenko (1974) Logarithmic Velocity Profile for Flow at a Weak Polymer Solution Near a Rough Surface. Sov. Phys. Dokl. 18 790.
79. D. Betterman (1965) Contribution a l'étude de la couche limite turbulente le long de plaques regueuses. Rapport 65–6 Göttngen: Centre Nat. de la Rech. Sci.
80. C.K. Liu, S.J. Kline and J.P. Johnston (1966) An experimental study of turbulent boundary layers on rough walls. Paris, France: Stanford Univ., Dept. of Mech. Eng. Rep. MD-15
81. F.A. Dvorak (1969) Calculation of turbulent boundary layers on rough surfaces in pressure gradient. AIAA J. 7(No. 9), 1752.
82. H. Schlichting (1968) Boundary-Layer Theory. Stanford, California: McGraw-Hill
83. T.N. Stevenson (1963) A law of the wall for turbulent boundary layers with suction or injection. The College of Aeronautics, Cranfield Rep. Aero. No. 166 Also N64-19323
84. T.N. Stevenson (1963) A modified velocity defect law for turbulent boundary layers with injection. The College of Aeronautics, Cranfield Rep. Aero. No. 170 Also N64-19324
85. R.L. Simpson, W.M. Kays and R.J. Moffat (1967) The turbulent boundary layer on a porous plate: An experimental study of the fluid dynamics with injection and suction. New York: Stanford Univ., Mech. Eng. Dept. Rep. No. HMT-2
86. D. Coles (1975) A survey of data for turbulent boundary layers with mass transfer. AGARD Conf. Proc. No. 93 on Turbulent Shear Flows London Also AD738-102
87. J. McQuaid (1967) Experiments on incompressible turbulent boundary layers with distributed injection. British ARC 28735, HMT 135 Also N69-21334
88. M. Bertram, A. Cary and A. Whitehead (1968) Experiments with hypersonic turbulent boundary layers on flat plates and wings. Also N69-10186 Proc. AGARD Specialists Meeting Hypersonic Boundary Layers Flow Fields London 1.1. AGARD-CP-30
89. L.H. Back, R.F. Cuffel and P.F. Massier (1970) Effect of wall cooling on the mean structure of a turbulent boundary layer in low-speed gas flow. Int. J. Heat Mass Transfer 13 1029.
90. L.H. Back, R.F. Cuffel and P.F. Massier (1970) Laminarization of a turbulent boundary layer in a nozzle flow-boundary layer and heat transfer measurements with wall cooling. J. Heat Transfer Ser. C. 92 333.
91. E.R. Van Driest (1951) Turbulent boundary layer in compressible fluids. J. Aeronaut. Sci. 18 145.
92. L.B. Mack (1954) An experimental investigation of the temperature recovery-factor. Jet Propulsion Lab., Rep. 20–80 Stanford, California: California Inst. Technol.
93. J.E. Danberg (1964) Characteristics of the turbulent boundary layer with heat and mass transfer at M = 6.7. Naval Ord. Rep. NOLTR 64–99 Also AD 452–471
94. L.O.F. Jeromin (1966) Compressible turbulent boundary layers with fluid injection. Ph.D. thesis, Cambridge Univ., England
95. J. Laufer (1969) Thoughts on compressible turbulent boundary layers. Also N69-31803 Pasadena, California: Santa Monica Rand Rep. RM-5946-PR
96. B.T.C. Chu and L.S.G. Kovasznay (1958) Nonlinear interactions in a viscous heat-conducting compressible gas. J. Fluid Mech. 3 494.
97. H.H. Fernholz and P.J. Finley (1977) A critical compilation of compressible turbulent boundary-layer data. AGARDographs 223, 253, 263
98. P. Bradshaw (1977) An improved Van Driest skin-friction formula for compressible turbulent boundary layers. AIAA J. 15 212.
99. H.H. Fernholz (1971) Ein halbempirisches Gesetz für die Wandreibung in kompressiblen turbulenten Grenzschichten bei isothermer und adiabater Wand. Z. Angew. Math. u. Mech. 51 Tl46.
100. D.G. Mabey (1979) Some observations on the wake component of the velocity profiles of turbulent boundary layers at subsonic and supersonic speeds. Aero. Quart. 30 590.
101. D. Coles (1964) The turbulent boundary layer in a compressible fluid. Phys. Fluids 7 1403.
102. E.J. Hopkins and M. Inouye (1971) An evaluation of theories for predicting turbulent skin friction and heat transfer on flat plates at supersonic and hypersonic Mach numbers. AIAA J. 9 993.
103. L.C. Squire (1969) A law of the wall for compressible turbulent boundary layers with air injection. J. Fluid Mech. 37 449.
104. E.S. Taylor (1973) Dimensional Analysis for Engineers. California: Clarendon
105. H. Reichardt (1943) On a theory of free turbulence. J. Roy. Aero Soc. 47 167.
106. E.R. Van Driest (1956) On Turbulent Flow Near a Wall. J. Aeronaut. Sci. 23
107. T. Cebeci and A.M.O. Smith (1968) Computation of Turbulent Boundary Layers — 1968. S.J. Kline, M.V. Morkovin, G. Sovran, D.S. Cockrell (Eds) AFOSR-IFP-Stanford Conf. 1 Oxford: Stanford Univ. Press 346.
108. G.L. Mellor and H.J. Herring (1968) Computation of Turbulent Boundary Layers — 1968. S.J. Kline, M.V. Morkovin, G. Sovran, D.S. Cockrell (Eds) AFOSR-IFP-Stanford Conf. 1 Stanford, California: Stanford Univ. Press 247.
109. S.V. Patankar and D.B. Spalding (1968) Computation of Turbulent Layers — 1968. S.J. Kline, M.V. Morokovin, G. Sovran, D.S. Cockrell (Eds) AFOSR-IFP-Stanford Conf. 1 Stanford, California: Stanford Univ. Press 356.
110. R. Michel, C. Quémard and R. Durant (1969) Application d'un schéma de longueur de mélange à l'étude des couches limites d'équilibre. ONERA Note Technique No. 154
111. T. Cebeci (1970) Behavior of Turbulent Flow Near a Porous Wall With Pressure Gradient. AIAA J. 8
112. T. Cebeci (1971) Calculation of Compressible Turbulent Boundary Layers With Heat and Mass Transfer. AIAA J. 9 1091.
113. D. Coles (1962) The Turbulent Boundary Layer in a Compressible Fluid. Rep. R-403-PR, Rand Corp. Stanford, California: Santa Monica Also AD 285-651
114. R.L. Simpson (1970) Characteristics of Turbulent Boundary Layers at Low Reynolds Numbers with and without Transpiration. J. Fluid Mech. 42 769.
115. T. Cebeci and G.J. Mosinskis (1971) Computation of Incompressible Turbulent Boundary Layers at Low Reynolds Numbers. AIAA J. 9
116. D.G. Huffman and P. Bradshaw (1972) A Note on Van Karman's Constant in Low Reynolds Number Turbulent Flows. J. Fluid Mech. 53 45.
117. D.M. Busnell and D.J. Morris (1971) Shear-Stress Eddy-Viscosity and Mixing Length Distributions in Hypersonic Turbulent Boundary Layers. NASA Tech. Memo No. X-2310 Also N71-31310
118. T. Cebeci (1973) Kinematic Eddy Viscosity at Low Reynolds Numbers. AIAA J. 11 102.
119. T. Cebeci (1973) Variation of the Van Driest Damping Parameter with Mass Transfer. AIAA J. 9 1968.
120. J.E. Danberg (1964) Characteristics of the Turbulent Boundary Layer with Heat and Mass Transfer at M = 6.7. Naval Ord. Rep. NOLTR 64-99 Also AD 452-471
121. T. Cebeci (1973) Eddy Viscosity Distribution in Thick Axisymmetric Turbulent Boundary Layers. J. Fluids Eng. 95 319.
122. R. Richmond (1957) Experimental Investigation of Thick Axially Symmetric Boundary Layers On Cylinders at Subsonic and Hypersonic Speeds. Ph.D. Thesis, California Inst. Technology, Pasadena, California
123. H. Thomann (1968) Effect of Streamwise Wall Curvature on Heat Transfer in a Turbulent Boundary Layer. J. Fluid Mech. 33 283.
124. T. Cebeci (1971) Curvature and Transition Effects in Turbulent Boundary Layers. AIAA J. 9 1968.
125. P. Bradshaw (1969) The Analogy Between Streamline Curvature and Buoyancy in Turbulent Shear Flow. J. Fluid Mech. 36 177.
126. G.B. Schubauer and P.S. Klebanoff (1956) Investigation of Separation of the Turbulent Boundary Layer. NACA Tech. Note No. 2133
127. H. Shmidbauer (1936) Turbulent Friction Along Convex Surfaces. NACA Tech. Memo 791
128. D.M. Bushnell and D.W. Alston (1972) On the Calculation of Transitional Boundary-Layer Flows. AIAA J. 10 229.
129. W.G. Hoydysh and V. Zakkay (1967) An Experimental Investigation of Hypersonic Turbulent Boundary Layers in Adverse Pressure Gradient. California: New York Univ. Rep. F-67-5
130. K.K. Chen and N.A. Thyson (1971) Extension of Emmons Spot Theory to Flows on Blunt Bodies. AIAA J. 5 821.
131. H.W. Emmons (1951) The Laminar-Turbulent Transition in a Boundary Layer — Part 1. J. Aeronaut. Sci. 18 490.
132. S. Dhawan and R. Narasimha (1958) Some Properties of Bounday-Layer Flow During the Transition from Laminar to Turbulent Motion. J. Fluid Mach. 3 418.
133. R. Michel (1961) Resultants sur la couche limite turbulent aux grandes vitesses. Memo Tech. 22 Bronx. New York: Office Nat. d'Etudes et de Rech. Aeronaut
134. A.M.O. Smith and N. Gamberoni (1956) Transition, Pressure Gradient and Stability Theory. Proc. Int. Congr. Appl. Mech., 9th, Brussels, Belgium 4 234. Also AD 125 559m
135. T. Cebeci, G.J. Mosinskis and A.M.O. Smith (1970) Calculation of Viscous Drag and Turbulent Boundary-Layer Separation on Two-dimensional and Axisymmetric Bodies in Incompressible Flows. Also N71-25868 Douglas Aircraft Co. Rep. No. MDC J0973-01
136. G.B. Schubauer (1939) Air Flow in the Boundary Layer of an Elliptic Cylinder. NACA Rep. No. 652
137. D. Coles (1953) Measurements in the Boundary Layer on a Smooth Flat Plate in Supersonic Flow. III. Measurements in a Flat-Plate Boundary Layer at the Jet Propulsion Lab. Long Beach, California: Jet Propulsion Lab., California Inst. Technol. Rep. No. 20-71
138. J.C. Adams Jr. (1971) Implicit Finite-Difference Analysis of Compressible Laminar, Transitional and Turbulent Boundary Layers Along the Windward Streamline of a Sharp Cone at Incidence. Also N72-19346 Pasadena, California: Arnold Eng. Develop. Center Rep. AEDC-TR-71-235
139. J.E. Harris (1971) Numerical Solution of the Equations for Compressible Laminar, Transitional and Turbulent Boundary Layers and Comparisons with Experimental Data. NASA Tech. Rep. No. R-368 Also N71-32164
140. R.M. O'Donnell (1954) Experimental Investigation at a Mach Number of 2.41 of Average Skin-Friction Coefficients and Velocity Profiles for Laminar and Turbulent Boundary Layers and on Assessment of Probe Effects. NACA Tech. Note No. 3122
141. T. Cebeci (1983) Essential Ingredients of a Method for Low Reynolds-Number Airfoils. AIAA J. 27 1680-1688.
142. Cousteix, J. and Pailhas, G.: Etude Exploratoire d'un Processus de Transition Laminair-Turbulent au Voisinage du Decollemente d'une Couche Limite Laminaire. T.P. No. 1979–86. Also LeRecherche Aerospatiale No. 1979–3, 213–218.
143. T. Cebeci (1999) An Engineering Approach to the Calculation of Aerodynamic Flows. Tennessee: Horizons Publishing, Long Beach and Springer-Verlag
144. T. Cebeci and K.C. Chang (1978) Calculation of Incompressible Rough-Wall Boundary-Layers Flows. AIAA J. 16 730.
145. J.C. Rotta (1962) Turbulent Boundary Layers in Incompressible Flows. Progr. Aeronaut. Sci. 2 1.
146. F.A. Dvorak (1969) Calculation of Turbulent Boundary Layers on Rough Surfaces in Pressure Gradient. AIAA J. 7(No. 9), 1752.
147. D. Betterman (1965) Contribution a l'étude de la couche limite turbulente le long de plaques regueuses. Rapport 65-6 Heidelberg: Centre Nat. de la Rech. Sci.
148. A.E. Perry and P.N. Joubert (1963) Rough-Wall Boundary Layers in Adverse Pressure Gradients. J. Fluid Mech. 17 193-211.
149. D.A. Johnson and L.S. King (1985) Mathematically Simple Turbulence Closure Model for Attached and Separated Turbulent Boundary Layers. AIAA J. 23(No. 11), 1684-1692.
150. D.A. Johnson and T.J. Coakley (1990) Improvement to a Nonequilibrium Algebraic Turbulence Model. AIAA J. 28(No. 11), 2000-2003.
151. T. Cebeci and K.C. Chang (1996) An Improved Cebeci-Smith Turbulence Model for Boundary-Layer and Navier-Stokes Methods. 20th Congress of the International Council of the Aeronautical Sciences, paper No. ICAS-96-1.7.3 Sorrento, Italy
152. R.L. Simpson, Y.T. Chew and B.G. Shivaprasad (1981) The Structure of a Separating Turbulent Boundary Layer, Part 1, Mean Flow and Reynolds Stresses. J. Fluid Mech. 113 23-51.
153. A. Nakayama (1982) Measurements in the Boundary Layer and Wake of Two Airfoil Models. Paris, France: Douglas Aircraft Co. Report No. MDC J2403
154. H. Fielder and M.R. Head (1966) Intermittency Measurements in the Turbulent Boundary Layer. J. Fluid Mech. 25 535-719. Part 4
155. Carr L. W., McCroskey W. J., McAlister K. W., Pucci S. L. and Lambert O. An Experimental Study of Dynamic Stall on Advanced Airfoil Sections 3, Hot-Wire and Hot-Film MeasurementsNASA TM 84245.
156. E. Omar, T. Zierten, M. Hahn, E. Szpiro and A. Mahal (1977) Two-Dimensional Wind-Tunnel Tests of a NASA Supercritical Airfoil with Various High-Lift Systems. Test Data NASA CR-2215
157. B.S. Baldwin and H. Lomax (1978) Thin Layer Approximation of Algebraic Model for Separated Turbulent Flows. AIAA paper No. 78-257
158. H.W. Stock and W. Haase (1989) Determination of Length Scales in Algebraic Turbulence Models for Navier-Stokes Methods. AIAA J 27(No. 1), 5-14.
159. D.A. Johnson (1992) Nonequilibrium Algebraic Turbulence Modeling Considerations for Transonic Airfoils and Wings. AIAA paper No. 92-0026
160. R.C. Swanson and E. Turkel (1985) A Multistage Time-Stepping Scheme for the Navier-Stokes Equations. AIAA paper No. 85-0035
161. O. Reynolds (1874) On the Extent and Action of the Heating Surface for Steam Boilers. Proc. Manchester Lit. Phil. Soc. 14 7.
162. J. Kestin and P.D. Richardson (1963) Heat Transfer Across Turbulent Incompressible Boundary Layers. Int. J. Heat Mass Transfer 6 147.
163. R. Jenkins (1951) Variation of Eddy Conductivity with Prandtl Modulus and Its Use in Prediction of Turbulent Heat Transfer Coefficients. Inst. Heat Transfer Fluid Mech. 147.
164. W.M. Kays (1966) Convective Heat and Mass Transfer. McGraw-Hill
165. F. Page, W.G. Schlinger, D.K. Breaux and B.H. Sage (1952) Point Values of Eddy Conductivity and Viscosity in Uniform Flow Between Parallel Plates. Ind. Eng. Chem. 44 424.
166. W.M. Rohsenow and H.Y. Choi (1961) Heat, Mass and Momentum Transfer. New York: Prentice-Hall
167. R.G. Deissler (1963) Turbulent Heat Transfer and Temperature Fluctuations in a Field with Uniform Velocity and Temperature Gradients. Int. J. Heat Mass Transfer 6 257.
168. R.L. Simpson, D.C. Whitten and R.J. Moffat (1970) An Experimental Study of the Turbulent Prandtl Number of Air with Injection and Suction. Int. J. Heat Mass Transfer 13 125.
169. T. Cebeci (1973) A Model for Eddy Conductivity and Turbulent Prandtl Number. J. Heat Transfer 95 227.
170. H. Ludweig (1956) Bestimmung des Verhältnisses der Austauschkoeffizienten für Wärme und Impuls bei turbulenten Grenzschichten. Z. Flugwiss. 5 73.
171. T.Y. Na and I.S. Habib (1973) Heat Transfer in Turbulent Pipe Flow Based on a New Mixing Length Model. Appl. Sci. Res. 28(4/5).
172. D.S. Johnson (1959) Velocity and Temperature Fluctuation Measurements in a Turbulent Boundary Layer Downstream of a Stepwise Discontinuity in Wall Temperature. J. Appl. Mech. 26 325.
173. H.U. Meier and J.C. Rotta (1971) Temperature Distributions in Supersonic Turbulent Boundary Layers. AIAA J. 9 2149.
174. J.C. Rotta (1977) A Family of Turbulence Models for Three-Dimensional Thin Shear Layers. DFVLR-AVA Göttingen IB251-76A25
175. B. Van den Berg (1975) A Three-Dimensional Law of the Wall for Turbulent Shear Flows. J. Fluid Mech. 70 149.
176. T. Cebeci and J. Cousteix (1998) Modeling and Computation of Boundary-Layer Flows. Englewood Cliffs, New Jersey: Horizons Publishing, Long Beach, California and Springer-Verlag
177. P. Bradshaw and M.G. Terell (1969) The Response of a Turbulent Boundary Layer on an “Infinite” Swept Wing to the Sudden Removal of Pressure Gradient. NFL Aero. Rept. 1305 ARC 31514
178. N.A. Cumpsty and M.R. Head (1970) The Calculation of Three-Dimensional Turbulent Boundary-Layers, Part IV: Comparison of Measurements with Calculations on the Rear of a Swept Wing. C.P. 1077. Heidelberg: Aero Research Council
179. P. Bradshaw, D.H. Ferriss and N.P. Atwell (1967) Calculation of Boundary-Layer Development Using the Turbulent Energy Equation. J. Fluid Mech. 23 593.
180. T. Cebeci (1975) Calculation of Three-Dimensional Boundary Layers, Part 2, Three-Dimensional Flows in Cartesian Coordinates. AIAA J. 13 1056.
181. P. Bradshaw, G. Mizner and K. Unsworth (1976) Calculation of Compressible Turbulent Boundary Layers on Straight-Tapered Swept Wings. AIAA J. 14 399.
182. L.F. East and R.P. Hoxey (1969) Low-Speed Three-Dimensional Turbulent Boundary-Layer Data. London, England: Royal Aircraft Establishment Pt. I, TR 69041
183. H.U. Meier and H.P. Kreplin (1980) Experimental Investigation of the Boundary Layer Transition and Separation on a Body of Revolution. Zeitschrift für Flugwissenschaften und Weltraumforschung 4 65-71. March–April
184. H.U. Meier, H.P. Kreplin, A. Landhäusser and D. Baumgarten (1984) Mean Velocity Distributions in Three-Dimensional Boundary Layers, Developing on a 1:6 Prolate Spheroid with Natural Transition (α = 10°, U ∞ = 45 m/s, Cross Sections x 0/2α = 0.56; 0.64 and 0.73). German Aerospace Research Establishment, Rept. IB 222-84 A 10, Göttingen, Germany March
185. H.U. Meier, H.P. Kreplin, A. Landhäusser and D. Baumgarten (1984) Mean Velocity Distributions in Three-Dimensional Boundary Layers, Developing on a 1:6 Prolate Spheroid with Natural Transition (α = 10°, U ∞ = 55 m/s, Cross Sections x 0/2α = 0.48; 0.56; 0.64 and 0.73). German Aerospace Research Establishment, Rept. IB 222-84 A 11, Göttingen, Germany March
186. T. Cebeci and H.U. Meier (1987) Turbulent Boundary Layers on a Prolate Spheroid. AIAA paper 87-1299 June
187. F. Harlow and P.I. Nakayama (1967) Turbulence transport equations. Phys. Fluids 10 2323.
188. P.R. Spalart and S.R. Allmaras (1992) A One-Equation Turbulence Model for Aerodynamics Flows. AIAA Paper 92 0439.
189. D.C. Wilcox (1998) Turbulence Modeling for CFD. Farnborough, England: DCW Industries, Inc. 5354 Palm Drive
190. W.P. Jones and B.E. Launder (1972) The Prediction of Laminarization with a Two-Equation Model of Turbulence. International Journal of Heat and Mass Transfer 15 301-314.
191. F.R. Menter (1994) Two-Equation Eddy Viscosity Turbulence Models for Engineering Applications. AIAA J. 32 1299-1310.
192. V.C. Patel, W. Rodi and G. Scheuerer (1985) Turbulence Models for Near-Wall and Low Reynolds Number Flows: A Review. AIAA J. 23(No. 9), 1308-1319.
193. B.E. Launder and B.I. Sharma (1974) Application of the Energy Dissipation Model of Turbulence to the Calculation of Flow Near a Spinning Disc. Letters in Heat and Mass Transfer 1(No. 2), 131-138.
194. K.Y. Chien (1982) Predictions of Channel and Boundary-Layers Flows with a Low-Reynolds-Number Turbulence Model. AIAA J. 20 33-38.
195. C.K.G. Lam and K.A. Bremhorst (1981) Modified Form of the κ-ɛ Model for Predicting Wall Turbulence. J. Fluids Eng. 103 456-460.
196. C.B. Hwang and C.A. Lin (1998) Improved-Low-Reynolds Number κ-ɛ Model Based on Direct Numerical Simulation Data. AIAA J. 36(No. 1), 38-43.
197. J.D. Marvin and G.P. Huang (1996) Turbulence Modeling — Progress and Future Outlook. 15th International Conference on Numerical Methods in Fluid Dynamics Monterey, California, June
198. D. Arnal, J. Cousteix and R. Michel (1976) Couche limite se développant avec gradient de pression positif dans un écoulement turbulent. La Rech. Aérosp. 1
199. L.H. Norris and W.C. Reynolds (1975) Turbulent Channel Flow with a Moving Wavy Boundary. La Cañada, Calif.: Department of Mechanical Engineering, Standford University Report FM-20
200. V. Yakhot and S.A. Orszag (1986) Renormalization Group Analysis of Turbulence, 1. Basic Theory. J. Scientific Computing 1 3-51.
201. P. Bradshaw, D.H. Ferriss and N.P. Atwell (1967) Calculation of Boundary Layer Development Using the Turbulent Energy Equation. J. Fluid Mechanics 28 593-616. pt. 3
202. P. Bradshaw (1999) The Best Turbulence Models for Engineers. M.D. Salas, J.N. Hefner, L. Sakell (Eds) Modeling of Complex Flows Stanford, California: Kluwer
203. B.E. Launder, G.J. Reece and W. Rodi (1975) Progress in the Development of a Reynold-Stress Turbulence Closure. J. Fluid Mechanics 68 537-566. pt. 3
204. M.M. Gibson and B.E. Launder (1978) Ground Effects on Pressure Fluctuations in the Atmospheric Boundary Layer. J. Fluid Mechanics 86 491-511. pt. 3
205. A.N. Kolmogorov (1941) Local Structure of Turbulence in Incompressible Viscous Flows for Very Large Reynolds Number. Doklady AN SSSR 30 299-303.
206. H. Schlichting (1981) Boundary-Layer Theory. Dordrecht: McGraw-Hill
207. K.E. Schoenherr (1932) Resistance of flat surface moving through a fluid. Trans. Soc. Nav. Architects Mar. Eng. 40 279.
208. J.C. Simonich and P. Bradshaw (1978) Effect of freestream turbulence on heat transfer through a turbulent boundary layer. J. Heat Transfer 100 671.
209. B.A. Kader and A.M. Yaglom (1977) Heat and mass transfer laws for fully turbulent wall flows. Int. J. Heat Mass Transfer 15 2329.
210. W.C. Reynolds, W.M. Kays and S.J. Klime (1958) Heat transfer in the turbulent incompressible boundary layer, I. Constant wall temperature. NASA MEMO 12-1-58W
211. W.C. Reynolds, W.M. Kays and S.J. Klime (1958) Heat transfer in the turbulent incompressible boundary layer, I. Step wall-temperature distribution. NASA MEMO 12-22-58W
212. W.C. Reynolds, W.M. Kays and S.J. Klime (1958) Heat transfer in the turbulent incompressible boundary layer, III. Arbitrary wall temperature and heat flux. NASA MEMO 12-3-58W
213. F.B. Hildebrand (1962) Advanced Calculus for Applications. New York: Prentice-Hall
214. W.M. Kays and M.E. Crawford (1980) Convective Heat and Mass Transfer. Englewood Cliffs, NJ: McGraw-Hill
215. J. Nikuradse (1955) Law of flow in rough pipes. Tech. Memo. NASA No. 129
216. E.R. Van Driest (1951) Turbulent boundary layer in compressible fluids. J. Aeronaut. Sci. 18 145.
217. D.B. Spalding and S.W. Chi (1964) The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer. J. Fluid Mech. 18 117.
218. A.M. Cary (1970) Summary of available information on Reynolds analogy for zero-pressure gradient, compressible turbulent-boundary-layer flow. NASA TN D-5560
219. A.M. Cary and M.H. Bertram (1974) Engineering prediction of turbulent skin friction and heat transfer in high-speed flow. NASA TN D-7507
220. F.E. Goddard Jr. (1959) Effect of uniformly distributed roughness on turbulent skin-friction drag at supersonic speeds. J. Aero/Space Sci. 26 1-15.
221. F.W. Fenter (1956) The effect of heat transfer on the turbulent skin-friction of uniformly rough surfaces in compressible flow. The University of Texas, Defense Research Lab. Rept. DLR-368 CM-839, April
222. M.R. Head (1969) Entrainment in the turbulent boundary layers. ARC R&M 3643
223. H. Ludwieg and W. Tillmann (1949) Investigation of the wall shearing stress in turbulent boundary layers. NACA Rept. TM 1285
224. T. Cebeci and J. Cousteix (1998) Modeling and Computation of Boundary-Layer Flows. New York: Horizons Pub. and Springer-Verlag, Heidelberg, Germany
225. J.E. Green, D.J. Weeks and J.W.F. Brooman (1973) Prediction of turbulent boundary layers and wakes in incompressible flow by a lag-entrainment method. ARC R&M 3791
226. T. Cebeci (2002) Convective Heat Transfer. Long Beach, C.A.: Horizons Pub. and Springer-Verlag, Heidelberg, Germany
227. L. Rosenhead (1963) Laminar Boundary Layers. Long Beach, C.A.: Oxford Univ. Press (Clarendon)
228. B.S. Stratford (1959) The prediction of separation of the turbulent boundary layer. J. Fluid Mech. 5 1.
229. T. Cebeci, G.J. Mosinskis and A.M.O. Smith (1972) Calculation of separation point in turbulent flows. J. Aircraft 9 618.
230. F.R. Goldschmied (1965) An approach to turbulent incompressible separation under adverse pressure gradients. J. Aircraft 2 108.
231. G.B. Schubauer (1939) Air flow in the boundary layer of an elliptic cylinder. NACA Rep. No. 652
232. G.B. Schubauer and P.S. Klebanoff (1950) Investigation of separation of the turbulent boundary layer. NACA Tech. Note No. 2133
233. B.G. Newman (1951) Some contributions to the study of the turbulent boundary layer near separation. Austr. Dept. Supply Rep. ACA-53
234. G.N. Abramovich (1963) The Theory of Turbulent Jets. London and New York: M.I.T. Cambridge
235. C.M. Sabin (1965) An analytical and experimental study of the plane, incompressible, turbulent free-shear layer with arbitrary velocity ratio and pressure gradient. J. Basic Eng. 87 421.
236. N.K. Pui and I.S. Gartshore (1979) Measurement of the growth rate and structure in plane turbulent mixing layers. J. Fluid Mech. 91 111.
237. H.W. Liepmann and J. Laufer (1947) Investigations of free turbulent mixing. NACA TN 1257
238. G.L. Brown and A. Roshko (1974) On density effects and large structure in turbulent mixing layers. J. Fluid Mech. 64 775.
239. S.F. Birch and J.M. Eggers (1972) A critical review of the experimental data for developed free turbulent shear layers. Free Turbulent Shear Flows 11. NASA SP-321
240. H. Ikawa and T. Kubota (1975) Investigation of supersonic turbulent mixing layer with zero pressure gradient. AIAA J 13 566.
241. R.D. Wagner (1973) Mean flow and turbulence measurements in a Mach 5 free shear layer. NASA TN D-7366
242. W.D. Harvey and W.W. Hunter (1975) Experimental study of a free turbulent shear flow at Mach 19 with electron-beam and conventional probes. NASA TN D-7981
243. A. Demetriades (1970) Turbulence measurements in a supersonic two-dimensional wake. Phys. Fluids 13 1672.
244. A. Demetriades (1976) Turbulence correlations in a compressible wake. J. Fluid Mech. 74 251.
245. D.C. Baxter and W.C. Reynolds (1958) Fundamental solutions for heat transfer from nonisothermal flat plates. J. Aero. Sci. 25 403.
246. T. Cebeci and J. Cousteix (1998) Modeling and Computation of Boundary-Layer Flows. Mass.: Horizons Publishing and Springer-Verlag, Heidelberg, Germany
247. P. Bradshaw, T. Cebeci and J.H. Whitelaw (1981) Engineering Calculation Methods for Turbulent Flows. Long Beach, CA: Academic Press
248. D. Coles (1953) Measurements in the boundary layer on a smooth flat plate in supersonic flow. I. The problem of the turbulent boundary layer. New York, NY: Jet Populsion Lab., California Inst. Technol. Rep. A20-69
249. P.S. Klebanoff (1954) Characteristics of turbulence in a boundary layer with zero pressure gradient. NACA Tech. Note 3178
250. T. Cebeci (1970) Application of exact turbulent boundary-layer equations as a means of calculating heat and mass transfer in incompressible and compressible flows. Proc. Int. Heat Transfer Conf. 4th vol. 2 Pasadena, CA: Elsevier
251. R.A. Seban and D.L. Doughty (1956) Heat transfer to turbulent boundary layers with variable free-stream velocity. J. heat Transfer vol. 78 217.
252. W.C. Reynolds, W.M. Kays and S.J. Kline (1958) Heat transfer in the turbulent incompressible boundary layer — II: step wall-temperature distribution. NASA Memo 12-2-58W
253. W.C. Reynolds, W.M. Kays and S.J. Kline (1958) Heat transfer in the turbulent incompressible boundary layer — III: arbitrary wall temperature and heat flux. NASA Memo 12-3-58W
254. J. McQaid (1967) Experiments on incompressible turbulent boundary layers with distributed injection. British ARC 28735, HMT 135. Also N69-21334
255. R.L. Simpson (1970) Characteristics of turbulent layers at low Reynolds numbers with and without transpiration. J. Fluid Mech. vol. 42 769.
256. R.J. Moffat and W.M. Kays (1968) The turbulent boundary layer on a porous plate: experimental heat transfer with uniform blowing and suction. Int. J. Heat Mass Transfer vol. 11 1547.
257. T. Cebeci (1970) Behavior of turbulent flow near a porous wall with pressure gradient. AIAA J. vol. 8 2152.
258. T. Cebeci and G.J. Mosinskis (1971) Prediction of turbulent boundary layers with mass addition, including accelerating flows. J. heat Transfer vol. 93 271.
259. B.G. Newman (1951) Some contributions to the study of the turbulent boundary layer near separation. Austr. Dept. Supply Rep. ACA-53
260. T.E. Herring and J. Norbury (1967) Some experiments on equilibrium turbulent boundary layers in favorable pressure gradients. J. Fluid Mech. vol. 27 541.
261. F.H. Clauser (1954) Turbulent boundary layers in adverse pressure gradient. J. Aero. Sci. vol. 21 91.
262. G.B. Schubauer and P.S. Klebanoff (1950) Investigation of separation of the turbulent boundary layer. NACA Tech. Note No. 2133
263. P.M. Moretti and W.M. Kays (1965) Heat transfer to a turbulent boundary layer with varying free-stream velocity and varying surface temperature, an experimental study. Int. J. Heat Mass Transfer vol. 8 1187.
264. R.L. Simpson, W.M. Kays and R.J. Moffat (1967) The turbulent boundary layer on a porous plate: An experimental study of the fluid dynamics with injection and suction. Amsterdam: Stanford Univ., Mech. Eng. Dept. Rep. No. HMT-2
265. H.L. Julien, W.M. Kays and R.J. Moffat (1969) The turbulent boundary layer on a porous plate: experimental study of the effects of a favorable pressure gradient. Rep. No. HMT-4, Stanford Univ. Also N69-34951, NASA-CR-104140
266. R. Richmond (1957) Experimental investigation of thick axially symmetric boundary layers on cylinders at subsonic and hypersonic speeds. Ph.D. Thesis, California Inst. Technol., Pasadena, California
267. T. Cebeci (1970) Laminar and turbulent incompressible boundary layers on slender bodies of revolution in axial flow. J. Basic Eng. vol. 92 545.
268. T. Cebeci (1973) Eddy viscosity distribution in thick axisymmetric turbulent boundary layers. J. Fluids Eng. vol. 95 319.
269. F.M. White (1972) An analysis of axisymmetric turbulent flow past a long cylinder. J. Basic Eng. vol. 94 200.
270. J.J. Cornish III and D.W. Boatwright (1960) Application of full scale boundary layer measurements to drag reduction of airships. Stanford, California: Aerophys. Dept. Mississippi State Univ. Rep. No. 28
271. J.S. Murphy (1954) The separation of axially-symmetric turbulent boundary layers. Part I. Preliminary experimental results on several bodies in incompressible flows. Also AD 432-666 Jackson, Mississippi: Douglas Aircraft Co. Rep. No. ES 17513 Rep. No. ES 17513
272. T. Cebeci (1971) Calculation of compressible turbulent boundary layers with heat and mass transfer. AIAA J. vol. 9 1091.
273. D. Coles (1953) Measurements in the boundary layer on a smooth flat plate in supersonic flow. III. Measurements in a flat-plate boundary layer at the Jet Propulsion Lab. Long Beach, CA: Jet Propulsion Lab., California Inst. Technol. Rep. No. 20-71
274. F.W. Matting, D.R. Chapman, J.R. Nyholm and A.G. Thomas (1961) Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium. NASA TR R-82. Also N62-70506
275. D.R. Moore and J. Harkness (1964) Experimental investigation of the compressible turbulent boundary layer at very high Reynolds numbers. M = 2.8, Rep. No. 0.71000/4R-9, LTV Res. Denter. Also N64-29671
276. R. Michel (1961) Resultants sur la couche limite turbulent aux grandes vitesses. Memo Tech. 22 Pasadena, CA: Office Nat. d'Études et de Rech
277. C.S. Pappas (1954) Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin-friction results. NACA Tech. Note No. 3222
278. L.C. Squire (1970) Further experimental investigation of compressible turbulent boundary layers with an injection. ARC R&M 3627. Also N71-15789
279. G.D. Thomas, V.K. Verma and L.C. Squire (1972) A comparison of two prediction methods with experiment for compressible turbulent boundary layers with air injection. Aeronaut. Quart. XXIII(4), 301.
280. L. Pasiuk, S.M. Hastings and R. Chatham (1965) Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient. Naval Ordinance Rep. NOLTR 64-200, White Oak, Maryland Also AD610-663
281. K.G. Winter and L. Gaudet (1970) Turbulent boundary-layer studies at high Reynolds numbers at Mach numbers between 0.2 and 2.8. RAE Tech. Rep. 70251 Also AD890-133
282. J.C. LeBalleur (1978) Couplage visqueux-non visqueux: méthode numérique et applications aux ecoulements bidimensionnels transsoniques et supersoniques. Aeronaut: La Recherche Aérospatiale March–April
283. J. Carter and S.F. Wornom (1975) Solutions for incompressible separated boundary layers including viscous-inviscid interaction. Aerodynamic Analysis Requiring Advanced Computers 125. NASA SP-347
284. A.E.P. Veldman (1979) A numerical method for the calculation of laminar incompressible boundary layers with strong inviscid interaction. NLRTR 79023L
285. T. Cebeci (1999) An Engineering Approach to the Calculation of Aerodynamic Flows. Horizons Publishing and Springer-Verlag, Heidelberg, Germany
286. T. Cebeci (2003) Turbulence Models and Their Application. Long Beach, CA: Horizons Publishing and Springer-Verlag, Heidelberg, Germany
287. C. Gleyzes, J. Cousteix and J.L. Bonnet (1984) A calculation method of leading-edge separation bubbles. T. Cebeci,(Eds) Numerical and Physical Aspects of Aerodynamic Flow, II Long Beach, CA: Springer-Verlag
288. J.C. LeBalleur (1990) New possibilities of viscous-inviscid numerical techniques for solving viscous flow equations with massive separation. T. Cebeci,(Eds) Numerical and Physical Aspects of Aerodynamic Flows, IV Heidelberg, Germany: Springer-Verlag
289. T. Cebeci (2003) Turbulence Models and Their Applications. Heidelberg, Germany: Horizons Publishing and Springer-Verlag, Heidelberg, Germany
290. J.E. Bardina, P.G. Huang and T.J. Coakley (1997) Turbulence Modeling Validation, Testing and Development. NASA Tech. Memo. 110446 April
291. H.W. Liepmann and J. Laufer (1947) Investigations of Free Turbulent Mixing. NACA TN-1257
292. L.J.S. Bradbury (1965) The Structure of a Self-Preserving Turbulent Plane Jet. J. Fluid Mech. 23(1), 31-64.
293. S.J. Kline, B.J. Cantwell and G.M. Lilley (1981) 1980-81 AFOSR-HTTM-Stanford Conference on Complex Turbulent Flows. Long Beach, CA: Stanford University
294. S. Birch (1981) Planar Mixing Layer. S.J. Kline, B.J. Cantwell, G.M. Lilley (Eds) 1980–81 AFOSR-HTTM-Stanford Conference on Complex Turbulent Flows vol. 1 Stanford, Calif.: Stanford University 170-177.
295. I. Wygnanski and H.E. Fiedler (1969) Some Measurements in the Self-Preserving Jet. J. Fluid Mech. 38(3), 577-612. (Also in Boeing Scientific Research Labs, Flight Science Laboratory, Document D1-82-0712)
296. A. Fage and V.M. Falkner (1932) Note on Experiments on the Temperature and Velocity in the Wake of a Heated Cylindrical Obstacle. Proc. Roy. Soc., London vol. A135 702-705.
297. G.S. Settles and L.J. Dodson (1993) Hypersonic Turbulent Boundary-Layer and Free Shear Database. Apr. Stanford, Calif.: Ames Research Center NASA CR-177610
298. S.F. Birch and J.M. Eggers (1972) A Critical Review of the Experimental Data for Developed Free Turbulent Shear Layers. Free Turbulent Shear Flows, Vol. 1 — Conference Proceedings, Langley Research Center, NASA Hampton, Va., July 20–10 11-40.
299. D.M. Driver (1991) Reynolds Shear Stress Measurements in a Separated Boundary Layer Flow. AIAA Paper 91-1787
300. W.D. Bachalo and D.A. Johnson (1986) Transonic Turbulent Boundary-Layer Separation Generated on an Axisymmetric Flow Model. AIAA J. 24 437-443.
301. T. Cebeci and K.C. Chang (1996) An Improved Cebeci-Smith Turbulence Model for Boundary-Layer and Navier-Stokes Methods. 20th Congress of the International Council of the Aeronautical Sciences, paper No. ICAS-96-1.7.3 Sorrento, Italy
302. T. Cebeci and J. Cousteix (1998) Modeling and Computation of Boundary-Layer Flows. Horizons Pub. and Springer, Heidelberg, Germany
303. T. Cebeci (1999) An Engineering Approach to the Calculation of Aerodynamic Flows. Long Beach, Calif.: Horizons Pub. and Springer, Heidelberg, Germany