Unsteady Unified Hypersonic-Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity

Unsteady Unified Hypersonic-Supersonic Aerodynamics: Analytical and Expedient Methods for Stability and Aeroelasticity

Author(s):

Publication title:

A collection of technical papers : 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : 11th AIAA/ASME/AHS Adaptive Structures Forum : 4th AIAA Gossamer Spacecraft Forum : AIAA Dynamics Specialists Conference, Norfolk, Virginia, 7-10 April 2003

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2003

Pub. Year:

2003

Vol.:

v. 7

No.:

2003-1964

Paper no.:

AIAA-2003-1964

Page(from):

5138

Page(to):

5155

Pages:

18

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563476259 [1563476258]

Language:

English

Call no.:

A07400/031401 (v.7)

Type:

Technical Paper

Details

TDL ID:	ZA00001570
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Forum ; AIAA Gossamer Spacecraft Forum ; AIAA Dynamics Specialists Conference
Conf. info. (Number):	44th ; 11th ; 4th
Conf. info. (Venue):	Norfolk, Virginia
Conf. info. (Date):	2003.04.07-2003.04.10

Similar Items:

1 Technical Paper CRITICAL EVALUATION OF THE UNSTEADY AERODYNAMICS APPROACH TO DYNAMIC STABILITY AT HIGH ANGLES OF ATTACK Final Hui, W.H. National Aeronautics and Space Administration	7 Technical Paper Unsteady Sonic Aerodynamics Using Acceleration Potential Approach Chen, P., Liu, D. American Institute of Aeronautics and Astronautics
2 Technical Paper Nonlinear Aeroelasticity and Unsteady Aerodynamics. Dowell, E., Tang, D. American Institute of Aeronautics and Astronautics	8 Technical Paper Gas-Kinetic Scheme for Hypersonic Plasma Aerodynamics Tang, L., Zheng, Y., Liu, D. American Institute of Aeronautics and Astronautics
3 Technical Paper Unified Computation Method of Unsteady Supersonic/Hypersonic Flow Past Two Dimensional Flat Plate and Rectangular Wings Jing-song,Chen, Han-min,Yang, Cai-wen,Zhang "Society of Automotive Engineering, Inc."	9 Technical Paper Effect of Underwing Store Aerodynamics on Analytically Predicted F-16 Aeroelastic Instability D. Maxwell, C. Denegri, K. Dawson, J. Dubben American Institute of Aeronautics and Astronautics
4 Technical Paper Random Aeroelastic Response due to Strong Hypersonic Unsteady-Wave/Shock Interaction with Acoustic Loads K. Kim, Y. Kim, M. Mignolet, D. Liu, P. Chen, D. Lee American Institute of Aeronautics and Astronautics	10 Technical Paper Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic Analysis Friedmann, P., Liu, L., Patt, D. American Institute of Aeronautics and Astronautics
5 Technical Paper A Study of Unsteady Hypersonic Segmented Projectile Aerodynamics Young,D., Goldstein,D. American Institute of Aeronautics and Astronautics	11 Technical Paper Effects of Unsteady and Viscous Aerodynamics on the Dynamics of a Flexible Air-breathing Hypersonic Vehicle M. Bolender, M. Oppenheimer, D. Doman American Institute of Aeronautics and Astronautics
6 Technical Paper ON THE LAGRANGIAN METHOD FOR STEADY AND UNSTEADY FLOW Hui., W.H. National Aeronautics and Space Administration	12 Technical Paper A unified aerodynamic-influence-coefficient approach for aeroelastic/aeroservoelastic and MDO applications Chen, P.C., Sarhaddi, D., Liu, D.D., Karpel, M. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12