Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶

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100 1 ‡aBingham, Gene J.
245 1 0 ‡aSubsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶ / ‡cby Gene J. Bingham and Albert L. Braslow.
264 1 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1954.
300 ‡a10 pages : ‡billustrations ; ‡c27 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aNACA research memorandum ; ‡vL54B18a
500 ‡aOn front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 97. Effective Date; February 25, 1955 WHL."
500 ‡aOn front cover: "April 5, 1954."
504 ‡aIncludes bibliographical references (page 6).
538 ‡aMode of access: Internet.
650 7 ‡aAirplanes ‡xFuselage. ‡2fast ‡0(OCoLC)fst00803220
650 7 ‡afuselages. ‡2aat ‡0(CStmoGRI)aat300220318
650 0 ‡aAirplanes ‡xFuselage.
650 0 ‡aAirplanes ‡xWings, Swept-back ‡xHandling characteristics.
700 1 ‡aBraslow, Albert L.
710 2 ‡aLangley Aeronautical Laboratory.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095100783
CID ‡a101828689
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