-
4
-
-
84983107591
-
-
th Aerodynamic Ground Testing Conference, Seattle, WA, June
-
th Aerodynamic Ground Testing Conference, Seattle, WA, June 1990.
-
(1990)
Large-Amplitude High-Rate Roll Oscillation System for the Measurement of Non-Linear Airloads
-
-
Hanff, E.S.1
Kapoor, K.2
Anstey, C.R.3
Prini, A.4
-
8
-
-
85008267530
-
Lift Force of Delta Wings
-
Sept
-
Lee, M. and Ho, C. M., "Lift Force of Delta Wings," Appl. Mech. Rev., Vol. 43, No. 9, Sept. 1990, pp. 209-221.
-
(1990)
Appl. Mech. Rev
, vol.43
, Issue.9
, pp. 209-221
-
-
Lee, M.1
Ho, C.M.2
-
11
-
-
18144392299
-
Nonlinear Problems in Flight Dynamics Involving Aerodynamic Bifurcations
-
AGARD Conference Proceedings No. 386, Paper 25, May
-
Tobak, M. and Chapman, G. T., "Nonlinear Problems in Flight Dynamics Involving Aerodynamic Bifurcations," Unsteady Aerodynamics-Fundamentals and Applications to Aircraft Dynamics, AGARD Conference Proceedings No. 386, Paper 25, May 1985.
-
(1985)
Unsteady Aerodynamics-Fundamentals and Applications to Aircraft Dynamics
-
-
Tobak, M.1
Chapman, G.T.2
-
12
-
-
0028498390
-
State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack
-
Sept.-Oct
-
Goman, M. and Khrabrov, A., "State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack," Journal of Aircraft, Vol. 31, No. 5, Sept.-Oct. 1994, pp. 1109-1115.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.5
, pp. 1109-1115
-
-
Goman, M.1
Khrabrov, A.2
-
13
-
-
0041993346
-
-
NASA TM 109120, NASA Langley Research Center, Hampton, VA, May
-
Klein, V. and Noderer, K. D., "Modeling of Aircraft Unsteady Aerodynamic Characteristics: Part 1-Postulated Models," NASA TM 109120, NASA Langley Research Center, Hampton, VA, May 1994.
-
(1994)
Modeling of Aircraft Unsteady Aerodynamic Characteristics: Part 1-Postulated Models
-
-
Klein, V.1
Noderer, K.D.2
-
14
-
-
12944287093
-
-
NASA TM 110161, NASA Langley Research Center, Hampton, VA, Apr
-
Klein, V. and Noderer, K. D., "Modeling of Aircraft Unsteady Aerodynamic Characteristics: Part 2-Parameters Estimated from Wind Tunnel Data," NASA TM 110161, NASA Langley Research Center, Hampton, VA, Apr. 1995.
-
(1995)
Modeling of Aircraft Unsteady Aerodynamic Characteristics: Part 2-Parameters Estimated from Wind Tunnel Data
-
-
Klein, V.1
Noderer, K.D.2
-
15
-
-
2942730219
-
-
NASA TM-97-206276, NASA Langley Research Center, Hampton, VA, Dec
-
Klein, V., Murphy, P. C, Curry, T. J. and Brandon, J. M., "Analysis of Wind Tunnel Longitudinal Static and Oscillatory Data of the F-16XL Aircraft," NASA TM-97-206276, NASA Langley Research Center, Hampton, VA, Dec. 1997.
-
(1997)
Analysis of Wind Tunnel Longitudinal Static and Oscillatory Data of the F-16XL Aircraft
-
-
Klein, V.1
Murphy, P.C.2
Curry, T.J.3
Brandon, J.M.4
-
16
-
-
84890518823
-
-
Wright Laboratory TR-92-3053, Wright-Patterson AFB, OH, Aug
-
Presdorf, T. A., "Subsonic Aerodynamic Research Laboratory," Wright Laboratory TR-92-3053, Wright-Patterson AFB, OH, Aug. 1992.
-
(1992)
Subsonic Aerodynamic Research Laboratory
-
-
Presdorf, T.A.1
-
17
-
-
84889550546
-
Highlights of the IAR/WL Delta Wing Program
-
AIAA Atmospheric Flight Mechanics Conference, Baltimore, MD, Aug. unpublished
-
Jenkins, J. E. and Hanff, E. S., "Highlights of the IAR/WL Delta Wing Program," AIAA Workshop III-Delta Wings, AIAA Atmospheric Flight Mechanics Conference, Baltimore, MD, Aug. 1995, unpublished.
-
(1995)
AIAA Workshop III-Delta Wings
-
-
Jenkins, J.E.1
Hanff, E.S.2
-
18
-
-
84983121187
-
-
AIAA Paper 98-4520, AIAA Atmospheric Flight Mechanics Conference, Boston, MA, Aug
-
Addington, G. A. and Nelson, R. C., "The Correspondence between Flow-Field Structure and Critical States on a 65-Degree Delta Wing," AIAA Paper 98-4520, AIAA Atmospheric Flight Mechanics Conference, Boston, MA, Aug. 1998.
-
(1998)
The Correspondence between Flow-Field Structure and Critical States on a 65-Degree Delta Wing
-
-
Addington, G.A.1
Nelson, R.C.2
-
19
-
-
84983134062
-
-
AIAA Paper 97-3646, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug
-
Myatt, J. H., "Modeling the Rolling 65-Degree Delta Wing with Critical State Encounters," AIAA Paper 97-3646, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, Aug. 1997.
-
(1997)
Modeling the Rolling 65-Degree Delta Wing with Critical State Encounters
-
-
Myatt, J.H.1
-
21
-
-
84982318352
-
Vortex Breakdown Location over 65° Delta Wings-Empiricism and Experiment
-
AIAA Paper 98-2526, Albuquerque, NM, June
-
th AIAA Applied Aerodynamics Conference, Albuquerque, NM, June 1998.
-
(1998)
th AIAA Applied Aerodynamics Conference
-
-
Jobe, C.E.1
-
22
-
-
0030109752
-
Critical States and Flow Structure on a 65-Deg Delta Wing
-
Mar.-Apr
-
Jobe, C. E., Hsia, A. H., Jenkins, J. E. and Addington, G. A., "Critical States and Flow Structure on a 65-Deg Delta Wing," Journal of Aircraft, Vol. 33, No. 2, Mar.-Apr. 1996, pp. 347-352.
-
(1996)
Journal of Aircraft
, vol.33
, Issue.2
, pp. 347-352
-
-
Jobe, C.E.1
Hsia, A.H.2
Jenkins, J.E.3
Addington, G.A.4
-
23
-
-
10344233369
-
Dynamic Stall Effects and Applications to High Performance Aircraft
-
AGARD R-776, Hampton, VA, Mar
-
Brandon, J. M., "Dynamic Stall Effects and Applications to High Performance Aircraft," Special Course on Aircraft Dynamics at High Angles of Attack: Experiments and Modelling, AGARD R-776, Hampton, VA, Mar. 1991.
-
(1991)
Special Course on Aircraft Dynamics at High Angles of Attack: Experiments and Modelling
-
-
Brandon, J.M.1
|