During process of entering planetary atmospheres, space vehicles may encounter largest flight dynamic pressures at very high Mach numbers; most severe aeroelastic phenomena may therefore occur at hypersonic speeds; 2 approximate techniques described hold promise of supplying information of dynamic airload prediction for 2- and 3-dimensional pointed bodies of general shape; illustrations including comparisons and application to chordwise divergence.
Dynamic airloads and aeroelastic problems at entry Mach numbers
J Aerospace Sciences
Journal of Aerospace Science ; 28 , n 3
1961
14 pages
Article (Journal)
English
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