Computational Aeroelastic Analysis of the Ares Crew Launch Vehicle During Ascent-Reference-Cited by-同舟云学术

Computational Aeroelastic Analysis of the Ares Crew Launch Vehicle During Ascent

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA Applied Aerodynamics Conference
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Author:

Bartels Robert¹,Chwalowski Pawel¹,Massey Steven¹,Heeg Jennifer¹,Mineck Raymond²,Wieseman Carol¹

Affiliation:

1. NASA Langley Research Center

2. ATK

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4374

Reference34 articles.

1. 1Hanson,P.W.andDoggett,R.V.J.“AerodynamicDampingandBuffetResponseofanAeroelasticModeloftheSaturnIBlockIILaunch Vehicle,”NASATechnicalNoteNASATND-2713,1965.

2. Aeroelastic Vehicle Dynamics of a Proposed Delta II 7920-10L Launch Vehicle

3. Aeroelastic instability caused by slender payloads.

4. Unsteady Flow Separation Can Endanger the Structural Integrity of Aerospace Launch Vehicles

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