Wind-tunnel investigation of the aerodynamic and structural-deflection characteristics of an inflatable airplane

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086 0 ‡aNAS 1.15:X-680
100 1 ‡aMcLemore, H. Clyde.
245 1 0 ‡aWind-tunnel investigation of the aerodynamic and structural-deflection characteristics of an inflatable airplane / ‡cby H. Clyde McLemore.
260 ‡aWashington, D.C. : ‡bGPO, ‡c1962.
300 ‡a202 p. : ‡bill., (chiefly tables) ; ‡c27 cm.
490 0 ‡aNASA TM ‡vno. X-680
500 ‡a"Report date August 1962."
504 ‡aIncludes bibliographic reference (p. 11).
520 3 ‡aTests were conducted in the Langley full-scale tunnel for a range of speeds from minimum stall speed to speeds at which it was possible to produce a load factor sufficient to cause wing buckling. Static aerodynamic and control data, wing-pressure-distribution data, wing-deflection photographs, and wing-guy-cable loads are presented. Results of the tests show that a maximum load factor of the order of 4.50 can be attained for a normal inflation pressure of 7.0 lb/sq in.
536 ‡aSponsored by National Aeronautics and Space Administration
538 ‡aMode of access: Internet.
650 0 ‡aStrains and stresses.
650 0 ‡aAirplanes ‡xWings ‡xTesting.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
710 2 ‡aGeorge C. Marshall Space Flight Center.
CID ‡a100075706
DAT 0 ‡a20101007164407.0 ‡b20141121000000.0
DAT 1 ‡a20180312185024.0 ‡b2023-10-04T18:01:29Z
DAT 2 ‡a2023-10-04T17:30:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lprepare.pl-004-007
FMT ‡aBK
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