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Applicability of an Analytical Shock/Expansion Solution to the Elevon Control Effectiveness for a 2-D Hypersonic Vehicle Configuration
AIAA Atmospheric Flight Mechanics Conference and Exhibit
◽
10.2514/6.2008-6384
◽
2008
◽
Author(s):
Torstens Skujins
◽
Carlos Cesnik
◽
Michael Oppenheimer
◽
David Doman
Keyword(s):
Hypersonic Vehicle
◽
Control Effectiveness
◽
Vehicle Configuration
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