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‡a(MiU)990128616300106381
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‡aY 3.N 21/5:15/A55C07
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‡aNACA RM A55C07
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‡aBray, Richard S.
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‡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.
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‡aFlight tests of a leading-edge area suction on a fighter-type airplane with a 35 degree swept-back wing.
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‡aWashington, D.C. :
‡bNational Advisory Committee for Aeronautics,
‡c[1955].
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‡a30 p. :
‡bill. ;
‡c27 cm.
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‡aNational Advisory Committee for Aeronautics research memorandum ;
‡vA55C07
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‡aNACA Research Memorandum A55C07.
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‡aOn front cover: "June 9, 1955."
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‡aTitle from cover.
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‡aIncludes bibliographical references: p. 12-13.
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‡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.
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‡aMode of access: Internet.
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‡aCharts, diagrams, etc.
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‡aWind tunnel testing.
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‡aAirplanes
‡xFlight testing.
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‡aBoundary layer control.
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‡aLeading edges (Aerodynamics)
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‡aAirplanes
‡xWings, Swept-back.
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‡aAirplanes
‡xWings.
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‡aSabre (Jet fighter plane)
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‡aAeronautics
‡xResearch.
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‡aInnis, Robert C.,
‡ejoint author.
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‡aUnited States.
‡bNational Advisory Committee for Aeronautics.
‡tNACA research memorandum.
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‡aAmes Research Center.
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‡aTechnical Report Archive & Image Library (TRAIL)
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‡a39015086432781
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