-
1
-
-
85087597151
-
Advanced Aerodynamic Design of Passive Porosity Control Effectors
-
8-11 January, Reno, NV. AIAA 2001-0249
-
Hunter, C. A., Viken, S. A., Wood, R. M., and Bauer, S. X. S.: Advanced Aerodynamic Design of Passive Porosity Control Effectors. 39' AIAA Aerospace Sciences Meeting and Exhibit, 8-11 January 2001, Reno, NV. AIAA 2001-0249.
-
(2001)
39' AIAA Aerospace Sciences Meeting and Exhibit
-
-
Hunter, C.A.1
Viken, S.A.2
Wood, R.M.3
Bauer, S.X.S.4
-
2
-
-
0005025602
-
-
AGARD-CP-365, May
-
Thiede, P., Krogmann, P., and Stanewsky, E., Active and Passive Shock/Boundary Layer Interaction Control On Supercritical Airfoils, AGARD-CP-365, May 1984.
-
(1984)
Active and Passive Shock/Boundary Layer Interaction Control On Supercritical Airfoils
-
-
Thiede, P.1
Krogmann, P.2
Stanewsky, E.3
-
4
-
-
84894437449
-
-
Rensselear Polytechnic Institute, Troy, NY, First Annual Report for NASA Grant No. NSG 1624. October 1, 1979 to September 30
-
Nagamatsu, H. T., Brower, W. B., Jr., Bahi, L.; and Marble, S. K., Investigation of Passive Shock Wave/Boundary Layer Control for Transonic Airfoil Drag Reduction, Rensselear Polytechnic Institute, Troy, NY, First Annual Report for NASA Grant No. NSG 1624. October 1, 1979 to September 30, 1980.
-
(1980)
Investigation of Passive Shock Wave/Boundary Layer Control For Transonic Airfoil Drag Reduction
-
-
Nagamatsu, H.T.1
Brower Jr., W.B.2
Bahi, L.3
Marble, S.K.4
-
5
-
-
0003292994
-
Suppression of Shocks on Transonic Airfoils
-
Sydney, August 19-22
-
Savu, G., Trifu, O., and Dumitrescu, L. Z., Suppression of Shocks on Transonic Airfoils, Proceedings of the International Symposium on Shock Tubes and Waves. Sydney, August 19-22, 1983.
-
(1983)
Proceedings of the International Symposium On Shock Tubes and Waves
-
-
Savu, G.1
Trifu, O.2
Dumitrescu, L.Z.3
-
6
-
-
0021457294
-
Porous Airfoils in Transonic Flow
-
July
-
Savu, G. and Trifu, O., Porous Airfoils in Transonic Flow, AIAA Journal, Vol. 22, No. 7, July 1984, pages 989-991.
-
(1984)
AIAA Journal
, vol.22
, Issue.7
, pp. 989-991
-
-
Savu, G.1
Trifu, O.2
-
7
-
-
0021317005
-
Porosity Effect on Supercritical Airfoil Drag Reduction by Shock Wave/Boundary Layer Control
-
June
-
Nagamatsu, H. T. and Orozco, R. D., Porosity Effect on Supercritical Airfoil Drag Reduction by Shock Wave/Boundary Layer Control, AIAA-84-1682, June 1984.
-
(1984)
AIAA-84-1682
-
-
Nagamatsu, H.T.1
Orozco, R.D.2
-
8
-
-
85001960765
-
Reduction of Cross-Flow Shock-Induced Separation with a Porous Cavity at Supersonic Speeds
-
June
-
Bauer, S. X. S. and Hernandez, G., Reduction of Cross-Flow Shock-Induced Separation with a Porous Cavity at Supersonic Speeds, AIAA-88-2567, June 1988.
-
(1988)
AIAA-88-2567
-
-
Bauer, S.X.S.1
Hernandez, G.2
-
9
-
-
24244437958
-
Assessment of Passive Porosity with Free And Fixed Separation on a Tangent-Ogive Forebody
-
Hilton Head, South Carolina, August 10-12, AIAA Paper No. 92-4494
-
Wood, R. ML;Banks. D W and Bauer S. X. S.: Assessment of Passive Porosity with Free And Fixed Separation on a Tangent-Ogive Forebody. Presented at the AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, August 10-12, 1992. AIAA Paper No. 92-4494.
-
(1992)
Presented At the AIAA Atmospheric Flight Mechanics Conference
-
-
Wood, R.M.1
Banks, D.W.2
Bauer, S.X.S.3
-
10
-
-
0028397253
-
Alleviation of Side Force on Tangent-Ogive Forebodies Using Passive Porosity
-
Bauer S X S. and Hemsch, M. J.: Alleviation of Side Force on Tangent-Ogive Forebodies Using Passive Porosity, Journal of Aircraft, Volume 31, Number 2, Pages 354-361, 1993.
-
(1993)
Journal of Aircraft
, vol.31
, Issue.2
, pp. 354-361
-
-
Bauer, S.X.S.1
Hemsch, M.J.2
-
11
-
-
0042727422
-
A Study of the Effects of Viscosity on Flow Over Slender Inclined bodies of Revolution
-
December
-
Allen, H. J. and Perkins, E. W., A Study of the Effects of Viscosity on Flow Over Slender Inclined bodies of Revolution, NACA TR 1048, December 1951.
-
(1951)
NACA TR 1048
-
-
Allen, H.J.1
Perkins, E.W.2
-
12
-
-
28844472905
-
A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip
-
July
-
Letko, W., A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip, NACA TN 2911, July 1953.
-
(1953)
NACA TN 2911
-
-
Letko, W.1
-
13
-
-
0012222721
-
Asymmetric Lateral-Directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack
-
November
-
Coe, P. L., Jr., Chambers, J. R., and Letko, W., Asymmetric Lateral-Directional Characteristics of Pointed Bodies of Revolution at High Angles of Attack, NASA TN D-7095, November 1972.
-
(1972)
NASA TN D-7095
-
-
Coe Jr., P.L.1
Chambers, J.R.2
Letko, W.3
-
15
-
-
85003319586
-
Occurrence and Inhibition of Large Yawing Moments During High Incidence Flight of Slender Missile Configurations
-
AIAA Paper 72-968, Sept
-
Clark, W. H. and Peoples, J. R., Occurrence and Inhibition of Large Yawing Moments During High Incidence Flight of Slender Missile Configurations, AIAA Paper 72-968, Sept. 1972.
-
(1972)
-
-
Clark, W.H.1
Peoples, J.R.2
-
16
-
-
4243772104
-
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0
-
December
-
Jorgensen, L. H. and Nelson, E. R., Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0, NASA TM X-3128, December 1974.
-
(1974)
NASA TM X-3128
-
-
Jorgensen, L.H.1
Nelson, E.R.2
-
17
-
-
4243772104
-
Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Side Strakes and Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0
-
March
-
Jorgensen, L. H. and Nelson, E. R., Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution With Side Strakes and Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0, NASA TM X-3130, March 1975.
-
(1975)
NASA TM X-3130
-
-
Jorgensen, L.H.1
Nelson, E.R.2
-
18
-
-
84894430038
-
Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0
-
February
-
Jorgensen, L. H. and Nelson, E. R., Experimental Aerodynamic Characteristics for Bodies of Elliptic Cross Section at Angles of Attack from 0° to 58° and Mach Numbers from 0.6 to 2.0, NASA TM X-3129, February 1975.
-
(1975)
NASA TM X-3129
-
-
Jorgensen, L.H.1
Nelson, E.R.2
-
19
-
-
84894426829
-
Aerodynamic characteristics of wing-body configuration with two advanced general aviation airfoil sections and simple flap systems
-
AugOl
-
Morgan, H. L. Jr. and Paulson, J. W., Jr.: Aerodynamic characteristics of wing-body configuration with two advanced general aviation airfoil sections and simple flap systems, NASA-TN-D-8524, AugOl, 1977.
-
(1977)
NASA-TN-D-8524
-
-
Morgan Jr., H.L.1
Paulson Jr., J.W.2
-
20
-
-
0027558061
-
Euler study on porous transonic airfoils with a view toward multipoint design
-
Apr 01
-
Hartwich P. M.: Euler study on porous transonic airfoils with a view toward multipoint design, Journal of Aircraft, Volume: 30 Issue: 2 Page: p. 184-191, Apr 01, 1993.
-
(1993)
Journal of Aircraft
, vol.30
, pp. 184-191
-
-
Hartwich, P.M.1
-
22
-
-
84983119248
-
Engine Face and Screen Loss Models for CFD Applications
-
AIAA Paper 97-2076, June
-
Bush, R. H.: Engine Face and Screen Loss Models for CFD Applications, AIAA Paper 97-2076, June 1997.
-
(1997)
-
-
Bush, R.H.1
-
23
-
-
85135735346
-
Losses in Flow Normal to Plane Screens
-
May
-
Cornell, W. G.: Losses in Flow Normal to Plane Screens, Transactions of the ASME, pp 791-799, May 1958.
-
(1958)
Transactions of the ASME
, pp. 791-799
-
-
Cornell, W.G.1
-
24
-
-
0004247668
-
-
Dover Publications, (originally published John Wiley and Sons, Inc., 1946)
-
Rouse, H., Elementary Mechanics of Fluids, Dover Publications, 1978 (originally published John Wiley and Sons, Inc., 1946), p57.
-
(1978)
Elementary Mechanics of Fluids
, pp. 57
-
-
Rouse, H.1
-
25
-
-
0025662592
-
Development of a Multigrid Code for 3-D Navier-Stokes Equations and its application to a grid-refinement Study
-
Vatsa, V.N. and Wedan, B.W.: Development of a Multigrid Code for 3-D Navier-Stokes Equations and its application to a grid-refinement Study. Computers and Fluids, Vol. 18, No. 4, pp 391-403, 1990.
-
(1990)
Computers and Fluids
, vol.18
, Issue.4
, pp. 391-403
-
-
Vatsa, V.N.1
Wedan, B.W.2
-
26
-
-
0003549341
-
Development of a flexible and efficient multigrid-based multiblock flow solver
-
AIAA Paper No. 93-0677, Jan
-
Vatsa, V.N., Sanetrik, M.D. and Parlette, E.B. Development of a flexible and efficient multigrid-based multiblock flow solver. AIAA Paper No. 93-0677, Jan. 1993
-
(1993)
-
-
Vatsa, V.N.1
Sanetrik, M.D.2
Parlette, E.B.3
-
28
-
-
2942757053
-
Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes
-
Roe, P.L., Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes, J. Comp. Phys., Vol. 43, No. 2, 1981, pp. 357-372.
-
(1981)
J. Comp. Phys
, vol.43
, Issue.2
, pp. 357-372
-
-
Roe, P.L.1
-
29
-
-
0020223604
-
Flux Vector Splitting for the Euler Equations
-
Van Leer, B., Flux Vector Splitting for the Euler Equations, Lecture Notes in Physics, Vol. 170, 1982, pp. 501-512.
-
(1982)
Lecture Notes In Physics
, vol.170
, pp. 501-512
-
-
van Leer, B.1
-
30
-
-
0003256550
-
Zonal Two Equation k-co Turbulence Models for Aerodynamic Flows
-
Menter, F.: Zonal Two Equation k-co Turbulence Models for Aerodynamic Flows, AIAA 93-2906, 1996.
-
(1996)
AIAA
, pp. 93-2906
-
-
Menter, F.1
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