-
1
-
-
84963496780
-
-
ICAS-94-7 2 1, 19th ICAS Conference, Anaheim
-
Francis, M.S., Henderson, E.D.; “X-31 Enhanced Fighter Maneuverability Demonstrator: Flight Test Achievements”, ICAS-94-7 2 1, 19th ICAS Conference, Anaheim, Sept 1994.
-
(1994)
X-31 Enhanced Fighter Maneuverability Demonstrator: Flight Test Achievements
-
-
Francis, M.S.1
Henderson, E.D.2
-
2
-
-
0020782413
-
Dynamics of Air Combat
-
Herbst, W.B., “Dynamics of Air Combat,” Journal of Aircraft, Vol. 20, July 1983.
-
(1983)
Journal of Aircraft
, vol.20
-
-
Herbst, W.B.1
-
5
-
-
0019046112
-
Future Fighter Technologies
-
Herbst, W.B.; “Future Fighter Technologies,” Journal or Aircraft. Vol. 17, August 1980.
-
(1980)
Journal Or Aircraft
, pp. 17
-
-
Herbst, W.B.1
-
6
-
-
84963580053
-
Supcrmancuverabiliiy
-
University of Virginia, Charlottesville, June
-
Herbst, W.B.; “Supcrmancuverabiliiy,” Joint Automatic Control Conference, University of Virginia, Charlottesville, June 17-19, 1981.
-
(1981)
Joint Automatic Control Conference
, pp. 17-19
-
-
Herbst, W.B.1
-
7
-
-
30244464369
-
-
McDonnell Aircraft Company, June 1990, WRDC Technical Report 90-6001, Restricted by Arms Export Control Act
-
Doave, P.M., Gay, C.H., Fligg, J.A., et.al.; “Multi-System Integrated Conlro] (MuSIC Program),” McDonnell Aircraft Company, June 1990, WRDC Technical Report 90-6001, Restricted by Arms Export Control Act.
-
Multi-System Integrated Conlro] (Music Program)
-
-
Doave, P.M.1
Gay, C.H.2
Fligg, J.A.3
-
8
-
-
30244577404
-
-
AG ARD-CP-520
-
Francis, M.S., Henderson, E.D., Kunz, E., et al., “X-31A Demonstration of Integrated Fl ight and Propulsion Control for Effective Combat at Extreme Angles of Attack,” AG ARD-CP-520, April 1993.
-
(1993)
X-31A Demonstration of Integrated Fl Ight and Propulsion Control for Effective Combat at Extreme Angles of Attack
-
-
Francis, M.S.1
Henderson, E.D.2
Kunz, E.3
-
11
-
-
0025505523
-
Combined Effects of Nose Bluntness and Surface Perturbations on Asymmetric Flow Past Slender Bodies
-
Moskovitz, C.A., Hall, R.M., and DeJarnette, F.R.; “Combined Effects of Nose Bluntness and Surface Perturbations on Asymmetric Flow Past Slender Bodies,” Journal of Aircraft, Vol. 27, No. 10, October 1990.
-
(1990)
Journal of Aircraft
, vol.10
, pp. 27
-
-
Moskovitz, C.A.1
Hall, R.M.2
Dejarnette, F.R.3
-
14
-
-
84889165148
-
A Status Report on High Alpha Technology Program (HATP) Ground Test to Flight Comparisons
-
NASA-DFRC, July
-
Hall, R.M., Banks, D.W., Fisher, D.F.; et al; “A Status Report on High Alpha Technology Program (HATP) Ground Test to Flight Comparisons,” 4th High Alpha Conference, NASA-DFRC, July 12-14, 1994.
-
(1994)
4Th High Alpha Conference
, pp. 12-14
-
-
Hall, R.M.1
Banks, D.W.2
Fisher, D.F.3
-
15
-
-
77956219249
-
-
AIAA 93-3451
-
Mendenhall, M.R., Perkins, S.C., and Ericcson, L.E.; “Prediction of Forebody Vortex-Induced Wing Rock on Wing-Body Configurations,” AIAA 93-3451, August 1993.
-
(1993)
Prediction of Forebody Vortex-Induced Wing Rock on Wing-Body Configurations
-
-
Mendenhall, M.R.1
Perkins, S.C.2
Ericcson, L.E.3
-
16
-
-
0024036423
-
Experimental Study of Effects of Forebody Geometry on High Angle-of-At-tack Stability,”
-
Brandon, J.M., Nguyen, L.T.; “Experimental Study of Effects of Forebody Geometry on High Angle-of-At-tack Stability,” Journal of Aircraft. Vol. 25, No 7. July 1988.
-
(1988)
Journal of Aircraft
, vol.25
, Issue.7
-
-
Brandon, J.M.1
Nguyen, L.T.2
-
17
-
-
5244331210
-
Wing Rock Suppression Using Forebody Vortex Control
-
Baltimore, MD
-
Ng, XT; “Wing Rock Suppression Using Forebody Vortex Control,” AIAA 9th Applied Aerodynamics Conference, Baltimore, MD, Sept 1991
-
(1991)
AIAA 9Th Applied Aerodynamics Conference
-
-
Ng, X.T.1
-
18
-
-
0011471911
-
-
NASATN D-8382
-
Carr, L.W., McAlister, K.W., and McCroskey, W.J.; “Analysis of the Development of Dynamic Stall Based on Oscillating Airfoil Experiments,” NASATN D-8382, Jan 1977.
-
(1977)
Analysis of the Development of Dynamic Stall Based on Oscillating Airfoil Experiments
-
-
Carr, L.W.1
McAlister, K.W.2
McCroskey, W.J.3
-
19
-
-
85003767545
-
Aerodynamic Loading on a Two-Dimensional Airfoil During Dynamic Stall
-
Ham, N.D.; “Aerodynamic Loading on a Two-Dimensional Airfoil During Dynamic Stall,” AIAA Journal. Vol. 6, Oct 1968.
-
(1968)
AIAA Journal
, vol.6
-
-
Ham, N.D.1
-
20
-
-
0022161618
-
Airfoil Dynamic Stall Performance with LargeAmpliiudc Motions
-
Francis, M.S., Kccsee, J.E.; “Airfoil Dynamic Stall Performance with LargeAmpliiudc Motions,” AIAA Journal, Vol. 23, No. 11, Nov 1985.
-
(1985)
AIAA Journal
, vol.23
, Issue.11
-
-
Francis, M.S.1
Kccsee, J.E.2
-
21
-
-
85001950381
-
Leading Edge Vortex Dynamics on a Pitching Delta Wing
-
Williamsburg, VA, June
-
Lemay, S.P., Batill, S.M., and Nelson, R.C.; “Leading Edge Vortex Dynamics on a Pitching Delta Wing,” AIAA 6th Applied Aerodynamics Conference, Williamsburg, VA, June 6-8, 1988
-
(1988)
AIAA 6Th Applied Aerodynamics Conference
, pp. 6-8
-
-
Lemay, S.P.1
Batill, S.M.2
Nelson, R.C.3
-
24
-
-
27844532760
-
-
AIAA 933674CP
-
Croom, M.A., Fratello, D.J., and Whipple, R.D.; “Dynamic Model Testing of the X31 Configuration for High Angle of Attack Flilght Dynamics Research,” AIAA 933674 CP, August 1993.
-
(1993)
Dynamic Model Testing of the X31 Configuration for High Angle of Attack Flilght Dynamics Research
-
-
Croom, M.A.1
Fratello, D.J.2
Whipple, R.D.3
-
26
-
-
84963490140
-
Comparsons of X-31 Flight, Wind Tunnel, and Yawing Moment Asymmetries at High Angles of Attack
-
NASA-DFRC, July
-
Cobieigh, B.R., Croom, B.R., and Tamrat, B.F.; “Comparsons of X-31 Flight, Wind Tunnel, and Yawing Moment Asymmetries at High Angles of Attack,” 4th High Alpha Conference, NASA-DFRC, July 12-14, 1994.
-
(1994)
4Th High Alpha Conference
, pp. 12-14
-
-
Cobieigh, B.R.1
Croom, B.R.2
Tamrat, B.F.3
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