STRUCTURAL DESIGN AND OPTIMISATION OF THE LAPCAT A2 MACH 5 VEHICLE BASED ON AERO-ELASTIC DEFORMATIONS
18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France
01.01.2012
10 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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