Linked Data Explorerhttp://worldcat.org/entity/work/id/890331463
A torsional stiffness criterion for preventing flutter of wings of supersonic missiles
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http://schema.org/about
- http://id.loc.gov/authorities/subjects/sh85049581
- http://id.worldcat.org/fast/928386
- http://id.worldcat.org/fast/852545
- http://id.worldcat.org/fast/798221
- http://id.loc.gov/authorities/subjects/sh85001301
- http://id.worldcat.org/fast/798241
- http://id.loc.gov/authorities/subjects/sh85001297
- http://id.worldcat.org/fast/1012163
- http://id.loc.gov/authorities/subjects/sh85136148
- http://id.loc.gov/authorities/subjects/sh85082139
- http://id.loc.gov/authorities/subjects/sh87002373
- http://id.worldcat.org/fast/1152860
http://schema.org/description
- "A formula, base on a semi-rational analysis, is presented for estimating the torsional stiffness necessary to prevent flutter of a sweptback uniform wing that attains supersonic speeds. Results of missile flights at speeds up to Mach number 1.4 demonstrate the usefulness of the formula."
http://schema.org/name
- "A torsional stiffness criterion for preventing flutter of wings of supersonic missiles"