Low-speed wind-tunnel investigation of various segments of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model

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050 ⊔ 4 ‡aTL521 ‡b.A3525 no. 8162
086 0 ⊔ ‡aNAS 1.14:D-8162
100 1 ⊔ ‡aCroom, Delwin R.
245 1 0 ‡aLow-speed wind-tunnel investigation of various segments of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model / ‡cDelwin R. Croom.
260 ⊔ ⊔ ‡aWashington : ‡bU.S. National Aeronautics and Space Administration, Langley Research Center ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1976.
300 ⊔ ⊔ ‡a[1], 23 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA technical note ; ‡vNASA TN D-8162
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 7).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aSpoilers (Airplanes) ‡xTesting.
650 ⊔ 0 ‡aAirplanes ‡xModels ‡xTesting.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
710 2 ⊔ ‡aLangley Research Center.
CID ⊔ ⊔ ‡a011443797
DAT 0 ⊔ ‡a20101105105104.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2025-01-02T19:13:48Z
DAT 2 ⊔ ‡a2025-01-02T18:30:02Z
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