-
1
-
-
0036086175
-
Aeroelastic response of a 2-D airfoil in compressible flight speed regimes exposed to blast loadings
-
Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Airfoil in Compressible Flight Speed Regimes Exposed to Blast Loadings," Aerospace Science and Technology, Vol. 6, No. 4, 2002, pp. 259-272.
-
(2002)
Aerospace Science and Technology
, vol.6
, Issue.4
, pp. 259-272
-
-
Marzocca, P.1
Librescu, L.2
Chiocchia, G.3
-
2
-
-
85087192296
-
Aeroelastic response of swept aircraft wings in a compressible flow field
-
AIAA Ppaper 2001-0714
-
Marzocca, P., Librescu, L., and Silva, W. A., "Aeroelastic Response of Swept Aircraft Wings in a Compressible Flow Field," AIAA Ppaper 2001-0714, 39th AIAA Aerospace Sciences Meeting, January 8-11, 2001, Reno, NV.
-
39th AIAA Aerospace Sciences Meeting, January 8-11, 2001, Reno, NV
-
-
Marzocca, P.1
Librescu, L.2
Silva, W.A.3
-
3
-
-
0004230787
-
-
Dover Publications, Inc., New York, NY
-
Bisplinghoff, R.L., Ashley, H., and Halfman, R. L., Aeroelasticity, Dover Publications, Inc., New York, NY, 1996.
-
(1996)
Aeroelasticity
-
-
Bisplinghoff, R.L.1
Ashley, H.2
Halfman, R.L.3
-
4
-
-
0009234093
-
On the use of the indicial function concept in the analysis of unsteady motion of wings and wing-tail combinations
-
NASA R 1188
-
Tobak, M., "On the Use of the Indicial Function Concept in the Analysis of Unsteady Motion of Wings and Wing-Tail Combinations," NASA R 1188, 1954.
-
(1954)
-
-
Tobak, M.1
-
5
-
-
0018452920
-
Unsteady aerodynamic modeling for arbitrary motions
-
Edwards, J. W., Ashley, H., and Breakwell, J.V., "Unsteady Aerodynamic Modeling for Arbitrary Motions," AIAA Journal, Vol. 17, No. 4, 1979, pp. 365-374.
-
(1979)
AIAA Journal
, vol.17
, Issue.4
, pp. 365-374
-
-
Edwards, J.W.1
Ashley, H.2
Breakwell, J.V.3
-
6
-
-
0003625419
-
Finite state modeling of aeroelastic systems
-
NASA CR 2779
-
Vepa, R., "Finite State Modeling of Aeroelastic Systems," NASA CR 2779, 1977.
-
(1977)
-
-
Vepa, R.1
-
7
-
-
0020098320
-
Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling
-
Karpel M., "Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling," Journal of Aircraft, Vol. 19, No. 3, 1982, pp. 221-227.
-
(1982)
Journal of Aircraft
, vol.19
, Issue.3
, pp. 221-227
-
-
Karpel, M.1
-
8
-
-
0003982543
-
Flutter and oscillating air-force calculations for an airfoil in a two-dimensional supersonic flow
-
NACA TN 1158 and NACA TR 846, October
-
Garrick, I. E. and Rubinow, S. I., "Flutter and Oscillating Air-Force Calculations for an Airfoil in a Two-dimensional Supersonic Flow," NACA TN 1158 and NACA TR 846, October 1946.
-
(1946)
-
-
Garrick, I.E.1
Rubinow, S.I.2
-
9
-
-
0020102987
-
A new solution method for lifting surfaces in subsonic flow
-
Ueda, T., and Dowell, E. H., "A New Solution Method for Lifting Surfaces in Subsonic Flow," AIAA Journal, Vol. 20, No.3, 1982, pp. 348-355.
-
(1982)
AIAA Journal
, vol.20
, Issue.3
, pp. 348-355
-
-
Ueda, T.1
Dowell, E.H.2
-
10
-
-
85007685430
-
A doublet-lattice method for calculating lift distribution on oscillating surfaces in subsonic flows
-
Albano, E., and Rodden, W. P., "A Doublet-Lattice Method for Calculating Lift Distribution on Oscillating Surfaces in Subsonic Flows," AIAA Journal, Vol. 7, No. 2, 1969, pp. 279-285.
-
(1969)
AIAA Journal
, vol.7
, Issue.2
, pp. 279-285
-
-
Albano, E.1
Rodden, W.P.2
-
11
-
-
17444383268
-
Development of a nonlinear indicial model for maneuvering fighter aircraft
-
AIAA Paper 96-0896
-
Reisenthel, P. H., "Development of a Nonlinear Indicial Model for Maneuvering Fighter Aircraft," AIAA Paper 96-0896, 34th Aerospace Sciences Meeting, Reno, Nevada, January 1996.
-
34th Aerospace Sciences Meeting, Reno, Nevada, January 1996
-
-
Reisenthel, P.H.1
-
12
-
-
18144392299
-
Nonlinear problems in flight dynamics involving aerodynamic bifurcations
-
NASA TM 86706, March; November 1985
-
Tobak, M. and Chapman, G. T., "Nonlinear Problems in Flight Dynamics Involving Aerodynamic Bifurcations," NASA TM 86706, March 1985, pp. 1-15, AGARD Unsteady Aerodynamics-Fundamentals and Applications to Aircraft Dynamics, November 1985.
-
(1985)
AGARD Unsteady Aerodynamics-Fundamentals and Applications to Aircraft Dynamics
, pp. 1-15
-
-
Tobak, M.1
Chapman, G.T.2
-
13
-
-
0035218131
-
Aeroelastic response of a 2-D lifting surfaces to gust and arbitrary explosive loading signatures
-
Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Lifting Surfaces to Gust and Arbitrary Explosive Loading Signatures," International Journal of Impact Engineering, Vol. 25, No. 1, 2001, pp. 41-65.
-
(2001)
International Journal of Impact Engineering
, vol.25
, Issue.1
, pp. 41-65
-
-
Marzocca, P.1
Librescu, L.2
Chiocchia, G.3
-
15
-
-
0009232539
-
The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds
-
NACA TN 2403
-
Lomax, H., Heaslet, M. A., and Sluder, L., "The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds," NACA TN 2403, 1951.
-
(1951)
-
-
Lomax, H.1
Heaslet, M.A.2
Sluder, L.3
-
16
-
-
0009162870
-
Numerical determination of indicial lift of a two-dimensional sinking airfoil at subsonic mach numbers from oscillatory lift coefficients with calculations for mach number 0.7
-
NACA TN 2562, 1951 and NACA TN 2613
-
Mazelsky, B., "Numerical Determination of Indicial Lift of a Two-dimensional Sinking Airfoil at Subsonic Mach Numbers from Oscillatory Lift Coefficients with Calculations for Mach Number 0.7," NACA TN 2562, 1951 and NACA TN 2613, 1952.
-
(1952)
-
-
Mazelsky, B.1
-
17
-
-
0003949807
-
-
Cambridge, New York, Cambridge University Press; Cambridge aerospace series, 12
-
Leishman, J. G., Principles of Helicopter Aerodynamics, Cambridge, New York, Cambridge University Press, 2000, Cambridge aerospace series, 12.
-
(2000)
Principles of Helicopter Aerodynamics
-
-
Leishman, J.G.1
-
18
-
-
84958069581
-
Identification of aerodynamic indicial functions using flight data
-
AIAA Ppare 82-1375
-
Gupta, N. K., and Iliff, K. W., "Identification of Aerodynamic Indicial Functions Using Flight Data," AIAA Ppare 82-1375, AIAA Atmospheric Flight Mechanics Conference, 9th, San Diego, CA, August 1982.
-
AIAA Atmospheric Flight Mechanics Conference, 9th, San Diego, CA, August 1982
-
-
Gupta, N.K.1
Iliff, K.W.2
-
19
-
-
0034224009
-
Transonic and low-supersonic aeroelastic analysis of two degree of freedom airfoil with freeplay non-linearity
-
Kim, D. H. and Lee, I., "Transonic and Low-Supersonic Aeroelastic Analysis of Two Degree of Freedom Airfoil with Freeplay Non-linearity," Journal of Sound and Vibration, Vol. 234, No. 5, 2000, pp. 859-880.
-
(2000)
Journal of Sound and Vibration
, vol.234
, Issue.5
, pp. 859-880
-
-
Kim, D.H.1
Lee, I.2
-
20
-
-
0042289368
-
Fluid/structure coupled analysis of a 2-DOF airfoil using unstructured euler code
-
Kim, D. H., Park, Y. M, Lee, I., and Kwon, O. J., "Fluid/Structure Coupled Analysis of a 2-DOF Airfoil Using Unstructured Euler Code," Journal of The Korean Society for Aeronautical and Space Science, Vol. 29, No. 4, 2001, pp. 8-19.
-
(2001)
Journal of The Korean Society for Aeronautical and Space Science
, vol.29
, Issue.4
, pp. 8-19
-
-
Kim, D.H.1
Park, Y.M.2
Lee, I.3
Kwon, O.J.4
-
21
-
-
0036079219
-
Nonlinear aeroelastic computation of a wing with a finned-store using a parallel unstructured euler solver
-
AIAA Paper 2002-1289
-
Kim, D. H., Park, Y. M. Lee, I., and Kwon O. J., "Nonlinear Aeroelastic Computation of a Wing with a Finned-Store Using a Parallel Unstructured Euler Solver," 43rd AIAA/ASME/ASCE/AHS ASC Structures, Structural Dynamics, and Materials Conf. & Exhibit, Denver, Colorado, 22-25 April 2002, AIAA Paper 2002-1289.
-
43rd AIAA/ASME/ASCE/AHS ASC Structures, Structural Dynamics, and Materials Conf. & Exhibit, Denver, Colorado, 22-25 April 2002
-
-
Kim, D.H.1
Park, Y.M.2
Lee, I.3
Kwon, O.J.4
-
22
-
-
0040617394
-
Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed
-
NACA-TR-1128, January; also bound with NACA AR-39-1; Supersedes NACA-TN-2590, January 1952
-
Nelson H. C. and Berman J. H., "Calculations on the forces and moments for an oscillating wing-aileron combination in two-dimensional potential flow at sonic speed," NACA-TR-1128, January 1953, also bound with NACA AR-39-1, pp. 469-484. Supersedes NACA-TN-2590, January 1952.
-
(1953)
, pp. 469-484
-
-
Nelson, H.C.1
Berman, J.H.2
-
23
-
-
0017932980
-
Computation of unsteady transonic flows by the indicial method
-
Ballhaus, W. F. and Goorjian, P. M., "Computation of Unsteady Transonic Flows by the Indicial Method," AIAA Journal, Vol. 16, No. 2, 1978, pp. 117-124.
-
(1978)
AIAA Journal
, vol.16
, Issue.2
, pp. 117-124
-
-
Ballhaus, W.F.1
Goorjian, P.M.2
-
24
-
-
4243782725
-
Some measurements of aerodynamic forces and moments at subsonic speeds on a rectangular wing of aspect ratio 2 oscillating about the midchord
-
NACA RM L53R19
-
Widmayer, E. Jr., Clevenson, S. A., and Leadbetter, S.A., "Some Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Rectangular Wing of Aspect Ratio 2 Oscillating About the Midchord," NACA RM L53R19, 1953.
-
(1953)
-
-
Widmayer E., Jr.1
Clevenson, S.A.2
Leadbetter, S.A.3
-
25
-
-
24244431698
-
Aerodynamic damping at mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method
-
NACA RM L56A26a
-
Tuovila, W. J. and Hess, R. W., "Aerodynamic Damping at Mach Numbers of 1.3 and 1.6 of a Control Surface on a Two-Dimensional Wing by the Free-Oscillation Method," NACA RM L56A26a, 1956.
-
(1956)
-
-
Tuovila, W.J.1
Hess, R.W.2
-
26
-
-
0038839483
-
Aerodynamic flutter coefficients for subsonic, sonic and supersonic flow (linear two-dimensional theory)
-
Reports and Memoranda No. 2932, April
-
Jordan, P. F., "Aerodynamic Flutter Coefficients for Subsonic, Sonic and Supersonic Flow (Linear Two-dimensional Theory)," Reports and Memoranda No. 2932, April 1953.
-
(1953)
-
-
Jordan, P.F.1
-
27
-
-
0039432084
-
Tables of coefficients for compressible flutter calculations
-
AF Technical Report No. 6200, August
-
Luke, Y. L., "Tables of Coefficients for Compressible Flutter Calculations," AF Technical Report No. 6200, August 1950.
-
(1950)
-
-
Luke, Y.L.1
-
28
-
-
0026626235
-
Transonic aeroelasticity analysis using state-space unsteady aerodynamic modeling
-
Crouse, G. and Leishman, J. G., "Transonic Aeroelasticity Analysis Using State-Space Unsteady Aerodynamic Modeling," AIAA Journal, Vol. 29, No. 1, 1992, pp. 153-160.
-
(1992)
AIAA Journal
, vol.29
, Issue.1
, pp. 153-160
-
-
Crouse, G.1
Leishman, J.G.2
-
29
-
-
85003347137
-
A strip method for prediction of damping in subsonic wind tunnel and flight flutter tests
-
Rodden, W. P. and Stahl, B., "A Strip Method for Prediction of Damping in Subsonic Wind Tunnel and Flight Flutter Tests," Journal of Aircraft, Vol. 6, No. 1, 1969, pp. 9-17.
-
(1969)
Journal of Aircraft
, vol.6
, Issue.1
, pp. 9-17
-
-
Rodden, W.P.1
Stahl, B.2
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