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070921s1967 dcua b 000 0 eng d |
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‡asdr-uiuc6394259
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‡a(OCoLC)173227599
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‡aEGM
‡cEGM
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‡aUIUU
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‡aTL573
‡b.B87 1967
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‡aBurk, Sanger M.
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‡aStatic aerodynamic characteristics of three ram-air-inflated low-aspect-ratio fabric wings /
‡cby Sanger M Burk, Jr. and George M. Ware.
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246 |
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‡aNASA TN D-4182
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‡aWashington, D. C. :
‡bNational Aeronautics and Space Administration ;
‡aSpringfield, Va. :
‡bfor sale by the Clearinghouse for Federal Scientific and Technical Information,
‡c1967.
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‡a34 p. :
‡bill. ;
‡c27 cm.
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‡aNASA technical note ;
‡vD-4182
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‡aIndludes bibliographical references (p. 10).
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‡aAn investigation of the low-speed static aerodynamic characteristics of three ram-air-inflated low-aspect-ratio fabric wings has been made in the Langley full-scale tunnel. The wings which were rectangular in planform and had an airfoil-shaped cross section were open at the nose to allow air to enter and inflate the wings; the payload was suspended on lines below the wings. Effects of four different test setups were also determined. The results indicated that the untrimmed maximum lift-drag ratios of the wings ranged from 1.9 to 2.7 and that the untrimmed maximum lift coefficients varied from about 0.9 to 1.1.
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‡aMode of access: Internet.
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‡aAerofoils.
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‡aOscillating wings (Aerodynamics)
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‡aAerodynamics.
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‡aWare, George M.
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‡aUnited States.
‡bNational Aeronautics and Space Administration.
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‡a011447479
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‡a20101104085213.0
‡b20141009010000.0
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‡a20141112165512.0
‡b2025-01-01T19:27:04Z
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‡a2025-01-01T18:30:02Z
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‡aSDR-UIUC
‡dUNKNOWN
‡lloader.pl-003-020
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‡aBK
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‡auiug
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‡puiug.30112106687103
‡sUIU
‡16394259
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‡bUIU
‡cUIUC
‡d20250101
‡sgoogle
‡uuiug.30112106687103
‡y1967
‡ric
‡qbib
‡tUS bib date1 >= 1930
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