Predictions of Store-Induced Limit-Cylce Oscillations Using Euler and Navier-Stokes Fluid Dynamics-Reference-Cited by-同舟云学术

Predictions of Store-Induced Limit-Cylce Oscillations Using Euler and Navier-Stokes Fluid Dynamics

Published:2003-04-07 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Snyder Richard,Scott James,Khot Narendra,Beran Philip,Zweber Jeffrey

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1727

Reference13 articles.

1. Eastep, F.E., and others, "Investigation of Shock-Induced LCO of a Wing/Store Configuration Using the Transonic Small Disturbance Method," Presented at the23rd Congress of the International Council of the Aeronautical Sciences (ICAS), September2002,Toronto,Canada.

2. Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections

3. Lewis, A.P., and Smith, M.J. "Euler-Based Aeroelastic Analysis of Shell Structures," Journal ofAircraft, Volume37,Number5,September2000, pp.840-845.

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