Prediction of aeroelastic effects for sea-skimming missiles with flow separation-Reference-Cited by-同舟云学术

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Prediction of aeroelastic effects for sea-skimming missiles with flow separation

Published:1991-04-08 Issue: Volume: Page:
ISSN:
Container-title:32nd Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

REISENTHEL P.¹,LESIEUTRE D.¹,NIXON D.¹

Affiliation:

1. Nielsen Engineering and Research, Inc., Mountain View, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1052

Reference15 articles.

1. 4atina,J. T.: An Efficient Algorithm for Solution of the UnsteadyTransonic SmallDisturbanceEquation, AIAA Paper 87-0109.

2. 5ixon,D., Caruso, S. C., and Klopfer, G. H.: Prediction of TransonicFlow withVortexEffects, AIAA Paper 90-0389.

3. 6eisenthel,P. and Nixon, D.: Prediction of Unsteady Separated Transonic Flow Around Missile Configurations,AIAAPaper 91-0601.

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1. Development of a nonlinear indicial model for maneuvering fighter aircraft;34th Aerospace Sciences Meeting and Exhibit;1996-01-15

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