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100075706 |
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20141121000000.0 |
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070403e196208 dcua bt f000 0 eng d |
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‡asdr-uiuc6365314
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‡a(OCoLC)122260470
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‡aFUG
‡cFUG
‡dLHL
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‡aUIUU
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‡aNAS 1.15:X-680
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‡aMcLemore, H. Clyde.
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‡aWind-tunnel investigation of the aerodynamic and structural-deflection characteristics of an inflatable airplane /
‡cby H. Clyde McLemore.
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‡aWashington, D.C. :
‡bGPO,
‡c1962.
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‡a202 p. :
‡bill., (chiefly tables) ;
‡c27 cm.
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‡aNASA TM
‡vno. X-680
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‡a"Report date August 1962."
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‡aIncludes bibliographic reference (p. 11).
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‡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.
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‡aSponsored by National Aeronautics and Space Administration
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‡aMode of access: Internet.
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‡aStrains and stresses.
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‡aAirplanes
‡xWings
‡xTesting.
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‡aUnited States.
‡bNational Aeronautics and Space Administration.
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‡aGeorge C. Marshall Space Flight Center.
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‡a100075706
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‡a20101007164407.0
‡b20141121000000.0
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‡a20180312185024.0
‡b2023-10-04T18:01:29Z
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‡a2023-10-04T17:30:02Z
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‡aSDR-UIUC
‡dUNKNOWN
‡lprepare.pl-004-007
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‡16365314
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‡bUIU
‡cUIUC
‡d20231004
‡sgoogle
‡uuiug.30112105148610
‡y1962
‡rpd
‡qbib
‡tUS fed doc
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