A QUASI-STEADY FLEXIBLE LAUNCH VEHICLE STABILITY ANALYSIS USING STEADY CFD WITH UNSTEADY AERODYNAMIC ENHANCEMENT
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
2011-01-01
13 pages
Includes bibliographical references and index
Conference paper
English
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Flexible Launch Vehicle Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics
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