Flight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing

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088 ‡aNACA RM A55C07
100 1 ‡aBray, Richard S.
245 1 0 ‡aFlight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree sweptback wing / ‡cRichard S. Bray and Robert C. Innis.
246 3 ‡aFlight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree swept-back wing.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c[1955].
300 ‡a30 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vA55C07
500 ‡aNACA Research Memorandum A55C07.
500 ‡aOn front cover: "June 9, 1955."
500 ‡aTitle from cover.
504 ‡aIncludes bibliographical references: p. 12-13.
520 3 ‡aTests have been made to determine the flight characteristics of an F-86F airplane equipped with a leading-edge area-suction boundary-layer-control system, and to investigate the possible operational limitations imposed on a fighter-type airplane by such an installation. The results of the flight tests are compared with those of full-scale wind-tunnel tests of a similar installation on a model incorporating F-86 wing panels. The basic porous-area distribution tested extended the full length of the wing leading edge. Suction power was provided by a modified turbosupercharger which was driven by air bled from the compressor of the airplane's jet engine.
538 ‡aMode of access: Internet.
650 0 ‡aCharts, diagrams, etc.
650 0 ‡aWind tunnel testing.
650 0 ‡aAirplanes ‡xFlight testing.
650 0 ‡aBoundary layer control.
650 0 ‡aLeading edges (Aerodynamics)
650 0 ‡aAirplanes ‡xWings, Swept-back.
650 0 ‡aAirplanes ‡xWings.
650 0 ‡aSabre (Jet fighter plane)
650 0 ‡aAeronautics ‡xResearch.
700 1 ‡aInnis, Robert C., ‡ejoint author.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. ‡tNACA research memorandum.
710 2 ‡aAmes Research Center.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015086432781
CID ‡a100167709
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