-
1
-
-
0041596039
-
The benchmark aeroelastic models program - Description and highlights of initial results
-
CP-507, AGARD, also NASA TM-104180
-
Bennett, R. M., Eckstrom, C. V., Rivera, J. A., Dansberry, B. E., Farmer, M. G., and Durham, M. H., "The Benchmark Aeroelastic Models Program - Description and Highlights of Initial Results," Transonic Unsteady Aerodynamics and Aeroelasticity, CP-507, AGARD, 1992; also NASA TM-104180, 1991.
-
(1991)
Transonic Unsteady Aerodynamics and Aeroelasticity
-
-
Bennett, R.M.1
Eckstrom, C.V.2
Rivera, J.A.3
Dansberry, B.E.4
Farmer, M.G.5
Durham, M.H.6
-
2
-
-
0342280888
-
-
AIAA Paper 91-1011, April 1991; also NASA TM-107582
-
Durham, M. H., Keller, D. F., Bennett, R. M., and Wieseman, C. D., "A Status Report on a Model for Benchmark Active Controls Testing," AIAA Paper 91-1011, April 1991; also NASA TM-107582, 1991.
-
(1991)
A Status Report on a Model for Benchmark Active Controls Testing
-
-
Durham, M.H.1
Keller, D.F.2
Bennett, R.M.3
Wieseman, C.D.4
-
3
-
-
0343150375
-
-
NASA TM-104211, July
-
Rivera, J. A., Jr., Dansberry, B. E., Durham, M. H., Bennett, R. M., and Silva, W. A., "Pressure Measurements on a Rectangular Wing with a NACA 0012 Airfoil During Conventional Flutter," NASA TM-104211, July 1992.
-
(1992)
Pressure Measurements on a Rectangular Wing with a NACA 0012 Airfoil During Conventional Flutter
-
-
Rivera J.A., Jr.1
Dansberry, B.E.2
Durham, M.H.3
Bennett, R.M.4
Silva, W.A.5
-
4
-
-
0142049250
-
-
AIAA Paper 92-2396, April 1992; also NASA TM-107581, March
-
Rivera, J. A., Dansberry, B. E., Bennett, R. M., Durham, M. H., and Silva, W. A., "NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions," AIAA Paper 92-2396, April 1992; also NASA TM-107581, March 1992.
-
(1992)
NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions
-
-
Rivera, J.A.1
Dansberry, B.E.2
Bennett, R.M.3
Durham, M.H.4
Silva, W.A.5
-
5
-
-
0042096920
-
-
AIAA 91-1010, 1991; also NASA TM-104072
-
Rivera, J. A., Dansberry, B. E., Farmer, M. G., Eckstrom, C. V., Seidel, D. A., and Bennett, R. M., "Experimental Flutter Boundaries with Unsteady Pressure Distributions for the NACA 0012 Benchmark Model," AIAA 91-1010, 1991; also NASA TM-104072, 1991.
-
(1991)
Experimental Flutter Boundaries with Unsteady Pressure Distributions for the NACA 0012 Benchmark Model
-
-
Rivera, J.A.1
Dansberry, B.E.2
Farmer, M.G.3
Eckstrom, C.V.4
Seidel, D.A.5
Bennett, R.M.6
-
6
-
-
0029219120
-
Summary of an active flexible wing program
-
Perry, B., III, Cole, S. R., and Miller, G. D., "Summary of an Active Flexible Wing Program," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 10-15.
-
(1995)
Journal of Aircraft
, vol.32
, Issue.1
, pp. 10-15
-
-
Perry B. III1
Cole, S.R.2
Miller, G.D.3
-
7
-
-
0013495487
-
-
NASA TR-R-450
-
Sandford, M. C., Abel, I., and Gray, D. L., "Development and Demonstration of a Flutter-Suppression System Using Active Controls," NASA TR-R-450, 1974.
-
(1974)
Development and Demonstration of a Flutter-Suppression System Using Active Controls
-
-
Sandford, M.C.1
Abel, I.2
Gray, D.L.3
-
8
-
-
84983208358
-
-
AIAA Paper 97-0829, Jan.
-
Scott, R. C., Hoadley, S. T., Wieseman, C. D., and Durham, M. H., "Benchmark Active Controls Technology Model Aerodynamic Data," AIAA Paper 97-0829, Jan. 1997; also Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 914-921.
-
(1997)
Benchmark Active Controls Technology Model Aerodynamic Data
-
-
Scott, R.C.1
Hoadley, S.T.2
Wieseman, C.D.3
Durham, M.H.4
-
9
-
-
0034275786
-
-
Scott, R. C., Hoadley, S. T., Wieseman, C. D., and Durham, M. H., "Benchmark Active Controls Technology Model Aerodynamic Data," AIAA Paper 97-0829, Jan. 1997; also Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 914-921.
-
(2000)
Journal of Guidance, Control, and Dynamics
, vol.23
, Issue.5
, pp. 914-921
-
-
-
10
-
-
0003832391
-
Compendium of unsteady aerodynamic measurements
-
Aug.
-
"Compendium of Unsteady Aerodynamic Measurements," AGARD Rept. 702, Aug. 1982.
-
(1982)
AGARD Rept. 702
-
-
-
11
-
-
0343736761
-
Compendium of unsteady aerodynamic measurements, addendum no. 1
-
May
-
"Compendium of Unsteady Aerodynamic Measurements, Addendum No. 1," AGARD Rept. 702, May 1985.
-
(1985)
AGARD Rept. 702
-
-
-
13
-
-
84964237806
-
Comparison of two Navier-Stokes aeroelastic methods using BACT benchmark experimental data
-
to be published
-
Bartels, R. E., and Schuster, D. M., "Comparison of Two Navier-Stokes Aeroelastic Methods Using BACT Benchmark Experimental Data," Journal of Guidance, Control, and Dynamics (to be published).
-
Journal of Guidance, Control, and Dynamics
-
-
Bartels, R.E.1
Schuster, D.M.2
-
15
-
-
0007374988
-
Application of the ENS3DAE/Navier-Stokes aeroelastic method
-
Paper 3 in Rept. 822, AGARD, March
-
Schuster, D. M., Beran, P. S., and Huttsell, L. J., "Application of the ENS3DAE/Navier-Stokes Aeroelastic Method," Numerical Unsteady Aerodynamics and Aeroelastic Simulation, Paper 3 in Rept. 822, AGARD, March 1998.
-
(1998)
Numerical Unsteady Aerodynamics and Aeroelastic Simulation
-
-
Schuster, D.M.1
Beran, P.S.2
Huttsell, L.J.3
-
16
-
-
0343301234
-
-
AAIA Paper 99-1469, Jan.
-
Roughen, K. M., Baker, M. L., and Fogarty, T., "CFD and Doublet-Lattice Calculation of Unsteady Control Surface Aerodynamics and Correlation with Wind-Tunnel Test," AAIA Paper 99-1469, Jan. 1999.
-
(1999)
CFD and Doublet-Lattice Calculation of Unsteady Control Surface Aerodynamics and Correlation with Wind-Tunnel Test
-
-
Roughen, K.M.1
Baker, M.L.2
Fogarty, T.3
-
20
-
-
0029747318
-
-
Society of Photo-Optical Instrumentation Engineers, Paper 2717-12, Feb.
-
Lichtenwalner, P., Little, G., and Scott, R., "Adaptive Neural Control of Aeroelastic Response," Society of Photo-Optical Instrumentation Engineers, Paper 2717-12, Feb. 1996.
-
(1996)
Adaptive Neural Control of Aeroelastic Response
-
-
Lichtenwalner, P.1
Little, G.2
Scott, R.3
-
21
-
-
0030398738
-
Adaptive neural control for active flutter suppression
-
Lichtenwalner, P., Little, G., Pado, L., and Scott, R., "Adaptive Neural Control for Active Flutter Suppression," Proceedings of the ASME Fluids Engineering Div. FED, Vol. 242, 1996.
-
(1996)
Proceedings of the ASME Fluids Engineering Div. FED
, vol.242
-
-
Lichtenwalner, P.1
Little, G.2
Pado, L.3
Scott, R.4
-
23
-
-
0010361384
-
-
Aeroelasticity Branch, NASA Langley Research Center, LWP-799, Hampton, VA, Sept.
-
"The Langley Transonic Dynamics Tunnel," Aeroelasticity Branch, NASA Langley Research Center, LWP-799, Hampton, VA, Sept. 1969.
-
(1969)
The Langley Transonic Dynamics Tunnel
-
-
-
24
-
-
1542606053
-
-
Royal Aeronautical Society, Paper 4, April
-
Cole, S. R., and Rivera, J. A., Jr., "The New Heavy Gas Testing Capability in the NASA Langley Transonic Dynamics Tunnel," Royal Aeronautical Society, Paper 4, April 1997.
-
(1997)
The New Heavy Gas Testing Capability in the NASA Langley Transonic Dynamics Tunnel
-
-
Cole, S.R.1
Rivera J.A., Jr.2
-
30
-
-
85069359510
-
-
AIAA Paper 80-0154, Jan.
-
Dougherty, N. S., Jr., and Fisher, D. F., "Boundary-Layer Transition on a 10-Deg Cone, Wind Tunnel/Flight Correlation," AIAA Paper 80-0154, Jan. 1980.
-
(1980)
Boundary-Layer Transition on a 10-Deg Cone, Wind Tunnel/Flight Correlation
-
-
Dougherty N.S., Jr.1
Fisher, D.F.2
-
31
-
-
0342866150
-
-
NASA TM-107734, March
-
Sleeper, R. K., Keller, D. F., Perry, B., III, and Sandford, M. C., "Characteristics of Vertical and Lateral Tunnel Turbulence Measured in Air in the Langley Transonic Dynamics Tunnel," NASA TM-107734, March 1993.
-
(1993)
Characteristics of Vertical and Lateral Tunnel Turbulence Measured in Air in the Langley Transonic Dynamics Tunnel
-
-
Sleeper, R.K.1
Keller, D.F.2
Perry B. III3
Sandford, M.C.4
-
34
-
-
0343736753
-
-
U.S Patent 4,475,385, 9 Oct. 1984
-
Farmer, M. G., "Mount System for Testing Flutter," U.S Patent 4,475,385, 9 Oct. 1984.
-
Mount System for Testing Flutter
-
-
Farmer, M.G.1
-
35
-
-
0343301231
-
-
NASA TM-4457, Sept.
-
Dansberry, B. E., Durham, M. H., Bennett, R. M., Turnock, D. L., Silva, W. A., and Rivera, J. A., Jr., "Physical Properties of the Benchmark Models Program Supercritical Wing," NASA TM-4457, Sept. 1993.
-
(1993)
Physical Properties of the Benchmark Models Program Supercritical Wing
-
-
Dansberry, B.E.1
Durham, M.H.2
Bennett, R.M.3
Turnock, D.L.4
Silva, W.A.5
Rivera J.A., Jr.6
-
36
-
-
0343736752
-
-
NASA CR-2543, May
-
Rowe, W. S., Redman, M. C., Ehlers, F. E., and Sebastian, J. D., "Prediction of Unsteady Aerodynamic Loadings Caused by Leading Edge and Trailing Edge Control Surface Motions in Subsonic Compressible Flow - Analysis and Results," NASA CR-2543, May 1975.
-
(1975)
Prediction of Unsteady Aerodynamic Loadings Caused by Leading Edge and Trailing Edge Control Surface Motions in Subsonic Compressible Flow - Analysis and Results
-
-
Rowe, W.S.1
Redman, M.C.2
Ehlers, F.E.3
Sebastian, J.D.4
-
37
-
-
0003814628
-
-
Air Force Flight Dynamics Lab., AFFDL-TR-71-5, Wright-Patterson AFB, OH, Nov.
-
Giesing, J. P., Kalman, T. P., and Rodden, W. P., "Subsonic Unsteady Aerodynamics for General Configurations, Part I - Vol. I - Direct Application of the Nonplanar Doublet Lattice Method," Air Force Flight Dynamics Lab., AFFDL-TR-71-5, Wright-Patterson AFB, OH, Nov. 1971.
-
(1971)
Subsonic Unsteady Aerodynamics for General Configurations, Part I - Vol. I - Direct Application of the Nonplanar Doublet Lattice Method
, vol.1
-
-
Giesing, J.P.1
Kalman, T.P.2
Rodden, W.P.3
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