-
1
-
-
34147156608
-
A Suggested Method for Analyzing for Transonic Flutter of Control Surfaces Based on Available Data
-
Erickson, A. L., and Stephenson, J. D., "A Suggested Method for Analyzing for Transonic Flutter of Control Surfaces Based on Available Data," NACA RM A7F30, 1947.
-
(1947)
NACA RM A7F30
-
-
Erickson, A.L.1
Stephenson, J.D.2
-
2
-
-
34548319928
-
-
Aircraft Research Council R & M
-
Lambourne, N. C., "Control Surface Buzz," Aircraft Research Council R & M, No. 3364, 1964.
-
(1964)
Control Surface Buzz
, Issue.3364
-
-
Lambourne, N.C.1
-
3
-
-
0343864321
-
A Numerical Study of Control Surface Buzz Using Computational Fluid Dynamics Methods
-
AIAA Paper 92-2654, June
-
Brase, L. O., Fuglsang, D. F., and Agarwal, S., "A Numerical Study of Control Surface Buzz Using Computational Fluid Dynamics Methods," AIAA Paper 92-2654, June 1992.
-
(1992)
-
-
Brase, L.O.1
Fuglsang, D.F.2
Agarwal, S.3
-
4
-
-
0348129533
-
Aeroelasticity of Nonconventional Airplane Configurations-Past and Future
-
Livne, E., and Weisshaar, T., "Aeroelasticity of Nonconventional Airplane Configurations-Past and Future," Journal of Aircraft, Vol. 40, No. 6, 2003, pp. 1047-1065.
-
(2003)
Journal of Aircraft
, vol.40
, Issue.6
, pp. 1047-1065
-
-
Livne, E.1
Weisshaar, T.2
-
5
-
-
0003508336
-
-
Cambridge Univ. Press, Cambridge, England, U. K, Chap. 19
-
Abzug, M., and Larrabee, E., Airplane Stability and Control - A History of Technologies That Made Aviation Possible, Cambridge Univ. Press, Cambridge, England, U. K., 1997, Chap. 19.
-
(1997)
Airplane Stability and Control - A History of Technologies That Made Aviation Possible
-
-
Abzug, M.1
Larrabee, E.2
-
7
-
-
0042678076
-
Benchmark Active Control Technology (BACT) Wing CFD Results, Verification an Validation Data for Computational Unsteady Aerodynamics
-
Oct
-
Schuster, D. M., and Bartels, R. E., "Benchmark Active Control Technology (BACT) Wing CFD Results," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO TR 26, Oct. 2000, pp. 225-238.
-
(2000)
RTO TR
, vol.26
, pp. 225-238
-
-
Schuster, D.M.1
Bartels, R.E.2
-
8
-
-
34548298200
-
Application of the Transpiration Method for Aeroservoelastic Prediction Using CFD
-
AIAA Paper 98-2071
-
Cole, H. S., Andrew, A. S., and Gupta, K., "Application of the Transpiration Method for Aeroservoelastic Prediction Using CFD," AIAA Paper 98-2071, 1998.
-
(1998)
-
-
Cole, H.S.1
Andrew, A.S.2
Gupta, K.3
-
9
-
-
34548322008
-
-
AIAA Paper 99-0766, Jan
-
Cole, H. S., Andrew, A. S., and Gupta, K., "CFD-Based Aeroservoelastic Predictions with Comparisons to Benchmark Experimental Data," AIAA Paper 99-0766, Jan. 1999.
-
(1999)
CFD-Based Aeroservoelastic Predictions with Comparisons to Benchmark Experimental Data
-
-
Cole, H.S.1
Andrew, A.S.2
Gupta, K.3
-
10
-
-
85006484589
-
Conservative Multizonal Interface Algorithm for the 3-D Navier-Stokes Equations
-
AIAA Paper 93-1601
-
Klopfer, G., and Molvik, G., "Conservative Multizonal Interface Algorithm for the 3-D Navier-Stokes Equations," AIAA Paper 93-1601, 1991.
-
(1991)
-
-
Klopfer, G.1
Molvik, G.2
-
11
-
-
0042176900
-
Virtual Zone Navier-Stokes Computations for Oscillating Control Surfaces
-
AIAA Paper 93-3363
-
Klopfer, G., and Obayashi, S., "Virtual Zone Navier-Stokes Computations for Oscillating Control Surfaces," AIAA Paper 93-3363, 1993.
-
(1993)
-
-
Klopfer, G.1
Obayashi, S.2
-
12
-
-
0004163847
-
Navier-Stokes Computations for Oscillating Control Surfaces
-
AIAA Paper 92-4431
-
Obayashi, S., and Guruswamy, G., "Navier-Stokes Computations for Oscillating Control Surfaces," AIAA Paper 92-4431, 1992.
-
(1992)
-
-
Obayashi, S.1
Guruswamy, G.2
-
13
-
-
0043179064
-
Navier-Stokes Computations on Full Span Wing Body Configuration for Oscillating Control Surfaces
-
AIAA Paper 93-3687
-
Obayashi, S., Chiu, I. T., and Guruswamy, G., "Navier-Stokes Computations on Full Span Wing Body Configuration for Oscillating Control Surfaces," AIAA Paper 93-3687, 1993.
-
(1993)
-
-
Obayashi, S.1
Chiu, I.T.2
Guruswamy, G.3
-
14
-
-
34548305515
-
Unsteady Control Surface Pressure Measurements and Computations
-
AIAA Paper 96-2417
-
Karlsson, A., and Winzell, B., "Unsteady Control Surface Pressure Measurements and Computations," AIAA Paper 96-2417, 1996.
-
(1996)
-
-
Karlsson, A.1
Winzell, B.2
-
15
-
-
34548357552
-
NAL SST Arrow Wing with Oscillating Flap, Verification an Validation Data for Computational Unsteady Aerodynamics
-
Oct
-
Matsushita, H., Tamayama, M., Saitoh, K., and Nakamichi, J., "NAL SST Arrow Wing with Oscillating Flap," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO TR 26, Oct, 2000, pp. 295-318.
-
(2000)
RTO TR
, vol.26
, pp. 295-318
-
-
Matsushita, H.1
Tamayama, M.2
Saitoh, K.3
Nakamichi, J.4
-
17
-
-
34147142821
-
Unsteady Shock Wave Motions on a Thin Airfoil at Transonic Speeds Caused by an Aileron Oscillation
-
AIAA, Reston, VA, 4-6 June
-
Weisshaar, T. A., Tamayama, M., and Nakamichi, J., "Unsteady Shock Wave Motions on a Thin Airfoil at Transonic Speeds Caused by an Aileron Oscillation," International Forum on Aeroelasticity and Structural Dynamics - Amsterdam, AIAA, Reston, VA, 4-6 June 2003.
-
(2003)
International Forum on Aeroelasticity and Structural Dynamics - Amsterdam
-
-
Weisshaar, T.A.1
Tamayama, M.2
Nakamichi, J.3
-
18
-
-
2942744681
-
Aeroelastic Analysis of an SST Typed Wing with a Trailing Edge Flap Using a Chimera Grid Approach
-
AIAA Paper 2004-1271
-
Utaka, Y., and Nakamichi, J., "Aeroelastic Analysis of an SST Typed Wing with a Trailing Edge Flap Using a Chimera Grid Approach," AIAA Paper 2004-1271, 2004.
-
(2004)
-
-
Utaka, Y.1
Nakamichi, J.2
-
19
-
-
48749145864
-
Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries
-
Osher, S., and Chakravarthy, S., "Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries," Journal of Computational Physics, Vol. 50, No. 3, 1983, pp. 447-481.
-
(1983)
Journal of Computational Physics
, vol.50
, Issue.3
, pp. 447-481
-
-
Osher, S.1
Chakravarthy, S.2
-
20
-
-
0004261656
-
Time Dependent Calculations Using Multigrid, with Applications to Unsteady Flows Past Airfoils and Wings
-
AIAA Paper 1991-1596, June
-
Jameson, A., "Time Dependent Calculations Using Multigrid, with Applications to Unsteady Flows Past Airfoils and Wings," AIAA Paper 1991-1596, June 1991.
-
(1991)
-
-
Jameson, A.1
-
21
-
-
0343228755
-
Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers
-
Badcock, K. J., Woodgate, M. A., and Richards, B. E., "Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers," Progress in Aerospace Sciences, Vol. 36, Nos. 5-6, 2000, pp. 351-392.
-
(2000)
Progress in Aerospace Sciences
, vol.36
, Issue.5-6
, pp. 351-392
-
-
Badcock, K.J.1
Woodgate, M.A.2
Richards, B.E.3
-
22
-
-
84985315986
-
Construction of Curvilinear Coordinate Systems and Applications to Mesh Generation
-
Gordon, W. J., and Hall, C. A., "Construction of Curvilinear Coordinate Systems and Applications to Mesh Generation," International Journal of Numerical Methods in Engineering, Vol. 7, No. 4, 1973, pp. 461-477.
-
(1973)
International Journal of Numerical Methods in Engineering
, vol.7
, Issue.4
, pp. 461-477
-
-
Gordon, W.J.1
Hall, C.A.2
-
23
-
-
0018529022
-
Geometric Conservation Law and Its Application to Flow Computations on Moving Grids
-
Thomas, P., and Lombard, C., "Geometric Conservation Law and Its Application to Flow Computations on Moving Grids," AIAA Journal, Vol. 17, No. 10, 1979, pp. 1030-1037.
-
(1979)
AIAA Journal
, vol.17
, Issue.10
, pp. 1030-1037
-
-
Thomas, P.1
Lombard, C.2
-
24
-
-
2542494783
-
Time Marching Analysis of Flutter Using Computational Fluid Dynamics,
-
Ph.D. Thesis, University of Glasgow, Glasgow, U.K
-
Goura, G. S. L., "Time Marching Analysis of Flutter Using Computational Fluid Dynamics," Ph.D. Thesis, University of Glasgow, Glasgow, U.K., 2001.
-
(2001)
-
-
Goura, G.S.L.1
-
25
-
-
34548300287
-
Test Cases for the Benchmark Active Controls Model: Spoiler and Control Surface Oscillations and Flutter, Verification an Validation Data for Computational Unsteady Aerodynamics
-
Oct
-
Scott, R. C., Bennett, R. M., and Wieseman, C. D., "Test Cases for the Benchmark Active Controls Model: Spoiler and Control Surface Oscillations and Flutter," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO TR 26, Oct. 2000, pp. 201-224.
-
(2000)
RTO TR
, vol.26
, pp. 201-224
-
-
Scott, R.C.1
Bennett, R.M.2
Wieseman, C.D.3
-
26
-
-
34548310644
-
Aeroelastic Analysis of Aircraft with Control Surfaces using CFD,
-
Ph.D. Thesis, University of Glasgow, Glasgow, U.K
-
Rampurawala, A. M., "Aeroelastic Analysis of Aircraft with Control Surfaces using CFD," Ph.D. Thesis, University of Glasgow, Glasgow, U.K., 2006.
-
(2006)
-
-
Rampurawala, A.M.1
|