Dynamic and aeroelastic problems encountered during ascent, orbit, re-entry and terminal phases of flight by maneuvering, lifting re-entry body are examined; similarities exist in buffet, aeroelastic and forced response problems for re-entry body; new facets of problems, involving thermal and hypersonic flow effects arising from flight profile and vehicle configuration, are assessed; recommendations made.
Dynamic and aeroelastic problems of lifting re-entry bodies
Aerospace Engineering
Aerospace Engineering ; 22 , n 1
1963
6 pages
Article (Journal)
English
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