-
1
-
-
84963905258
-
Operational benefits of Thrust Vector Control (TVC)
-
J.R. Chambers, W.P. Gilbert, and L.T. Nguyen, eds. NASA CP-3149
-
Bitten, R. and Selmon, J. “Operational benefits of Thrust Vector Control (TVC)”. High-Angle-of-Attack Technology, Volume I. J.R. Chambers, W.P. Gilbert, and L.T. Nguyen, eds. NASA CP-3149, Part 2, 1992.
-
(1992)
High-Angle-Of-Attack Technology
, vol.1
-
-
Bitten, R.1
Selmon, J.2
-
2
-
-
0019046112
-
Future Fighter Technologies
-
Herbst, W. B. “Future Fighter Technologies”. Journal of Aircraft, vol. 17, no.
-
Journal of Aircraft
, vol.17
-
-
Herbst, W.B.1
-
3
-
-
84963877706
-
-
August
-
August 1980.
-
(1980)
, Issue.8
-
-
-
4
-
-
0021938481
-
Propulsion Influences on Air Combat
-
85-1457, July
-
Herrick, P. W. “Propulsion Influences on Air Combat”. AIAA-85-1457, July 1985
-
(1985)
AIAA
-
-
Herrick, P.W.1
-
5
-
-
84997646339
-
Impact of Emerging Technologies on Future Combat Aircraft Agility
-
90-1304, May
-
Nguyen, L.T.N and Gilbert, W.P. “Impact of Emerging Technologies on Future Combat Aircraft Agility”. AIAA-90-1304, May 1990.
-
(1990)
AIAA
-
-
Nguyen, L.1
Gilbert, W.P.2
-
6
-
-
12944265887
-
Air Combat Payoffs of Vectoring/Reversing Exhaust Nozzles
-
88-3239, July
-
Herrick, P. W. “Air Combat Payoffs of Vectoring/Reversing Exhaust Nozzles”. ALAA-88-3239, July 1988.
-
(1988)
ALAA
-
-
Herrick, P.W.1
-
7
-
-
0010216736
-
Investigation of Thrust Vectoring and Post-Stall Capability in Air Combat
-
88-4160-CP
-
Costes, P. “Investigation of Thrust Vectoring and Post-Stall Capability in Air Combat”. AIAA-88-4160-CP, 1988.
-
(1988)
AIAA
-
-
Costes, P.1
-
8
-
-
0012387426
-
The Nonaxisymmetric Nozzle -It is for Real
-
79-1810, August
-
Capone, F. J. “The Nonaxisymmetric Nozzle -It is for Real” AIAA-79-1810, August 1979.
-
(1979)
AIAA
-
-
Capone, F.J.1
-
9
-
-
12944265886
-
Flight Test Results of the F-15 SMTD Thrust Vectoring/Thrust Reversing Exhaust Nozzle
-
90-1906, July
-
Bursey, R. and Dickinson, R. “Flight Test Results of the F-15 SMTD Thrust Vectoring/Thrust Reversing Exhaust Nozzle”. AIAA-90-1906, July 1990.
-
(1990)
AIAA
-
-
Bursey, R.1
Dickinson, R.2
-
10
-
-
12944335573
-
The F-18 High Alpha Research Vehicle: A High Angle-of-Attack Testbed Aircraft
-
104253
-
Regenie, V., Gatlin, D., Kempel, R., Matheny, N. “The F-18 High Alpha Research Vehicle: A High Angle-of-Attack Testbed Aircraft”. NASA TM-104253, 1992.
-
(1992)
NASA TM
-
-
Regenie, V.1
Gatlin, D.2
Kempel, R.3
Matheny, N.4
-
11
-
-
12944333518
-
X-31 Flight Test Update
-
92-1035, February
-
Knox, F., and Scellenger, H. “X-31 Flight Test Update”. AIAA-92-1035, February 1992.
-
(1992)
AIAA
-
-
Knox, F.1
Scellenger, H.2
-
12
-
-
84963494913
-
The Countercurrent Mixing Layer: Strategies for Shear-Layer Control
-
93-3260, July
-
Strykowski, P. J., and Krothapalli, A. “The Countercurrent Mixing Layer: Strategies for Shear-Layer Control”. AIAA 93-3260, July 1993.
-
(1993)
AIAA
-
-
Strykowski, P.J.1
Krothapalli, A.2
-
13
-
-
0027700312
-
Enhancement of Mixing in High-Speed Heated Jets Using a Counterflow Nozzle
-
November
-
Strykowski, P. J., Krothapalli, A., and Wishart, D. “Enhancement of Mixing in High-Speed Heated Jets Using a Counterflow Nozzle,” AIAA Journal Volume 31, number 11. November 1993.
-
(1993)
AIAA Journal
, vol.31
, Issue.11
-
-
Strykowski, P.J.1
Krothapalli, A.2
Wishart, D.3
-
14
-
-
84963787558
-
Experimental Study of a Nozzle Using Fluidic Counterflow Thrust Vectoring
-
Flamm, J.D. “Experimental Study of a Nozzle Using Fluidic Counterflow Thrust Vectoring”. AIAA 98-3255, July 1998.
-
(1998)
AIAA
, pp. 98-3255
-
-
Flamm, J.D.1
-
18
-
-
0001652995
-
Counterflow Thrust Vectoring of Supersonic Jets
-
96-0115, January
-
Strykowski, P. J., Krothapalli, A., and Forliti, D. J. “Counterflow Thrust Vectoring of Supersonic Jets”. AIAA 96-0115, January 1996.
-
(1996)
AIAA
-
-
Strykowski, P.J.1
Krothapalli, A.2
Forliti, D.J.3
-
19
-
-
0011494478
-
Numerical Simulation of Jet Aerodynamics Using a Three Dimensional Navier Stokes Method (PAB3D)
-
3596, September
-
Pao, S.P., and Abdol-Hamid, K.S. “Numerical Simulation of Jet Aerodynamics Using a Three Dimensional Navier Stokes Method (PAB3D)”. NASA TP-3596, September 1996.
-
(1996)
NASA TP
-
-
Pao, S.P.1
Abdol-Hamid, K.S.2
-
20
-
-
0007518152
-
Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D)
-
4702, December
-
Abdol-Hamid, K.S. “Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D)”. NASA CR-4702, December 1995.
-
(1995)
NASA CR
-
-
Abdol-Hamid, K.S.1
-
21
-
-
0006054653
-
Application of the Navier-Stokes Code PAB3D with k-e Turbulence Models to attached and Separated Flows
-
3480, January
-
Abdol-Hamid, K.S., Lakshmanan, B., and Carlson, J.R. “Application of the Navier-Stokes Code PAB3D with k-e Turbulence Models to attached and Separated Flows”. NASA TP-3480, January 1995.
-
(1995)
NASA TP
-
-
Abdol-Hamid, K.S.1
Lakshmanan, B.2
Carlson, J.R.3
-
22
-
-
84963884672
-
High Reynolds Number Analysis of Flat Plate and Separated Afterbody Flow Using Non-Linear Turbulence Models
-
96-2544, July
-
Carlson, J.R. “High Reynolds Number Analysis of Flat Plate and Separated Afterbody Flow Using Non-Linear Turbulence Models”. AIAA 96-2544, July 1996.
-
(1996)
AIAA
-
-
Carlson, J.R.1
-
23
-
-
0347371112
-
A New Reynolds Stress Algebraic Equation Model
-
106644, August
-
Shih, T.H., Zhu, J., and Lumley, J.L. “A New Reynolds Stress Algebraic Equation Model”. NASA TM-106644, August 1994.
-
(1994)
NASA TM
-
-
Shih, T.H.1
Zhu, J.2
Lumley, J.L.3
-
24
-
-
0012443524
-
Fully-Explicit and Self-Consistent Algebraic Reynolds Stress Model
-
95-82, December
-
Girimaji, S.S. “Fully-Explicit and Self-Consistent Algebraic Reynolds Stress Model”. ICASE 95-82, December 1995.
-
(1995)
ICASE
-
-
Girimaji, S.S.1
-
25
-
-
84876649972
-
Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows
-
98-3107, July
-
Hunter, C.A. “Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows”. AIAA 98-3107, July 1998.
-
(1998)
AIAA
-
-
Hunter, C.A.1
|