-
1
-
-
0004239276
-
Supercritical Wing Sections I, II, III
-
Springer-Verlag, New York
-
Bauer, F., Garabedian, P., Korn, D., and Jameson, A., “Supercritical Wing Sections I, II, III,” Lecture Notes in Economics and Mathematical Systems, Springer-Verlag, New York, 1972, 1975, 1977.
-
(1972)
Lecture Notes in Economics and Mathematical Systems
, vol.1975
, pp. 1977
-
-
Bauer, F.1
Garabedian, P.2
Korn, D.3
Jameson, A.4
-
2
-
-
0005120939
-
Theory of Viscous Transonic Flow Over Airfoils at High Reynolds Number
-
June
-
Melnik, R.E., Chow, R. R., and Mead, H. R., “Theory of Viscous Transonic Flow Over Airfoils at High Reynolds Number,” AIAA Paper 77-680, June 1977.
-
(1977)
AIAA Paper 77-680
-
-
Melnik, R.E.1
Chow, R.R.2
Mead, H.R.3
-
3
-
-
85003226868
-
-
Presented at the Conference on Low Reynolds Number Airfoil Aerodynamics, University of Notre Dame, Notre Dame, IN
-
Gleyzes, C., Cousteix, Jr., and Bonnet, J. L., “Theoretical and Experimental Study of Low Reynolds Number Transitional Separation Bubbles,” Presented at the Conference on Low Reynolds Number Airfoil Aerodynamics, University of Notre Dame, Notre Dame, IN, 1985.
-
(1985)
Theoretical and Experimental Study of Low Reynolds Number Transitional Separation Bubbles
-
-
Gleyzes, C.1
Cousteix, J.R.2
Bonnet, J.L.3
-
4
-
-
0021614962
-
Analysis of Airfoil Leading Edge-Separation Bubbles
-
Dec
-
Vatsa, V. N. and Carter, J. E., “Analysis of Airfoil Leading Edge-Separation Bubbles,” AIAA Journal, Vol. 22, Dec. 1984, pp. 1697-1704.
-
(1984)
AIAA Journal
, vol.22
, pp. 1697-1704
-
-
Vatsa, V.N.1
Carter, J.E.2
-
7
-
-
0021866244
-
Newton Solution of Direct and Inverse Transonic Euler Equations
-
July
-
Giles, M. B., Drela, M., and Thompson, W. T., “Newton Solution of Direct and Inverse Transonic Euler Equations,” AIAA Paper 85-1530, July 1985.
-
(1985)
AIAA Paper 85-1530
-
-
Giles, M.B.1
Drela, M.2
Thompson, W.T.3
-
8
-
-
0023421355
-
A Two-Dimensional Transonic Aerodynamic Design Method
-
Sept
-
Giles, M. B. and Drela, M., “A Two-Dimensional Transonic Aerodynamic Design Method,” AIAA Journal, Vol. 25, Sept. 1987, pp. 1199-12060.
-
(1987)
AIAA Journal
, vol.25
, pp. 1199-12060
-
-
Giles, M.B.1
Drela, M.2
-
9
-
-
85003364437
-
-
Presented at the Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan
-
Drela, M., Giles, M. B., and Thompkins, W. T., “Newton Solution of Coupled Euler and Boundary Layer Equations,” Presented at the Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan. 1985.
-
(1985)
Newton Solution of Coupled Euler and Boundary Layer Equations
-
-
Drela, M.1
Giles, M.B.2
Thompkins, W.T.3
-
10
-
-
85003357831
-
-
Presented at the Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan
-
Melnik, R. E. and Brook, J. W., “Computation of Viscid/In-viscid Interaction on Airfoils with Separated Flow,” Presented at the Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan. 1985.
-
(1985)
Computation of Viscid/In-Viscid Interaction on Airfoils with Separated Flow
-
-
Melnik, R.E.1
Brook, J.W.2
-
11
-
-
0019717538
-
Strong Matching Method for Computing Transonic Viscous Flows Including Wakes and Separations on Lifting Airfoils
-
English Ed
-
Le Balleur, J. C., “Strong Matching Method for Computing Transonic Viscous Flows Including Wakes and Separations on Lifting Airfoils,” La Recherche Aerospatiale, No. 1981-83, English Ed., 1981-83, pp. 21-45.
-
(1981)
La Recherche Aerospatiale
, Issue.1981-1983
, pp. 21-45
-
-
Le Balleur, J.C.1
-
12
-
-
0018529009
-
Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile
-
Whitfield, D. L., “Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile,” AIAA Paper 78-1158, 1978.
-
(1978)
AIAA Paper 78-1158
-
-
Whitfield, D.L.1
-
15
-
-
0020767526
-
Analytical Approximation of TwoDimensional Separated Turbulent Boundary-Layer Velocity Profiles
-
June
-
Swafford, T. W., “Analytical Approximation of TwoDimensional Separated Turbulent Boundary-Layer Velocity Profiles,” AIAA Journal, Vol. 21, June 1983, pp. 923-926.
-
(1983)
AIAA Journal
, vol.21
, pp. 923-926
-
-
Swafford, T.W.1
-
16
-
-
20544458689
-
Prediction of Turbulent Boundary Layers and Wakes in Compressible Flow by a Lag-Entrainment Method
-
HMSO, London, England
-
Green, J. E., Weeks, D. J. and Brooman, J.W.F., “Prediction of Turbulent Boundary Layers and Wakes in Compressible Flow by a Lag-Entrainment Method,” ARC R&M Rept. No. 3791, HMSO, London, England, 1977.
-
(1977)
ARC R&M Rept
, Issue.3791
-
-
Green, J.E.1
Weeks, D.J.2
Brooman, J.W.F.3
-
17
-
-
38349152399
-
Calculation of Boundary-Layer Development Using the Turbulent Energy Equation: Compressible Flow on Adiabatic Walls
-
Bradshaw, P. and Ferriss, D. H., “Calculation of Boundary-Layer Development Using the Turbulent Energy Equation: Compressible Flow on Adiabatic Walls,” Journal of Fluid Mechanics, Vol. 46, Pt. 1, 1970, pp. 83-110.
-
(1970)
Journal of Fluid Mechanics
, vol.46
, pp. 83-110
-
-
Bradshaw, P.1
Ferriss, D.H.2
-
18
-
-
0002447043
-
Turbulent Boundary Layers in Adverse Pressure Gradients
-
Feb
-
Clauser, F. H., “Turbulent Boundary Layers in Adverse Pressure Gradients,” Journal of Aeronautical Sciences, Vol. 21, Feb. 1954, pp. 91-108.
-
(1954)
Journal of Aeronautical Sciences
, vol.21
, pp. 91-108
-
-
Clauser, F.H.1
-
19
-
-
0003741690
-
-
Douglas Aircraft Co., Rept. ES 26388
-
Smith, A.M.O. and Gamberoni, N., “Transition, Pressure Gradient, and Stability Theory,” Douglas Aircraft Co., Rept. ES 26388, 1956.
-
(1956)
Transition, Pressure Gradient, and Stability Theory
-
-
Smith, A.M.O.1
Gamberoni, N.2
-
20
-
-
0004143477
-
-
Delft University of Technology, Dept, of Aerospace Engineering, Rept. VTH-74
-
Ingen, J. L. van, “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Delft University of Technology, Dept, of Aerospace Engineering, Rept. VTH-74, 1956.
-
(1956)
A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region
-
-
Ingen, J.L.V.1
-
21
-
-
85003221622
-
-
Presented at the Conference on Low Reynolds Number Airfoil Aerodynamics, University of Notre Dame, Notre Dame, IN, UNDAS-CP-77B123, June
-
Liebeck, R. H. and Camacho, P. P., “Airfoil Design at Low Reynolds Number with Constrained Pitching Moment,” Presented at the Conference on Low Reynolds Number Airfoil Aerodynamics, University of Notre Dame, Notre Dame, IN, UNDAS-CP-77B123, June 1985.
-
(1985)
Airfoil Design at Low Reynolds Number with Constrained Pitching Moment
-
-
Liebeck, R.H.1
Camacho, P.P.2
-
22
-
-
85040872599
-
-
AGARD Working Group 7, AGARD Rept. AR-211
-
Cook, P. H., McDonald, M. A., and Firmin, M.C.P., AGARD Working Group 7, “Test Cases for Inviscid Flow Field Methods,” AGARD Rept. AR-211, 1985.
-
(1985)
Test Cases for Inviscid Flow Field Methods
-
-
Cook, P.H.1
McDonald, M.A.2
Firmin, M.C.P.3
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