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ALUMINUM RUNWAY SURFACE AS POSSIBLE AID TO AIRCRAFT BRAKING

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BookPublisher: National Aeronautics And Space Administration,Washington, D.C. 1973Description: 31.DDC classification: NASA | TN D-7186

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-7186 (Browse shelf)	Not for loan		TR16897

Total holds: 0

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Previous	NASA TN D-7183 LOW-SPEED WIND-TUNNEL INVESTIGATION OF A SEMISPAN STOL JET TRANSPORT WING-BODY WITH AN UPPER-SURFACE BLOWN JET FLAP	NASA TN D-7184 A MULTISPECTRAL STUDY OF AN EXTRATROPICAL CYCLONE WITH NIMBUS 3 MEDIUM RESOLUTION INFRARED RADIOMETER DATA	NASA TN D-7185 THEORETICAL AND EXPERIMENTAL INTERNAL FLOW CHARACTERISTICS OF A-13.97-CENTIMETER-DIAMETER INLET AT STOL TAKEOFF AND APPROACH CONDITIONS	NASA TN D-7186 ALUMINUM RUNWAY SURFACE AS POSSIBLE AID TO AIRCRAFT BRAKING	NASA TN D-7187 PERFORMANCE OF AN ION-CYCLOTRON-WAVE PLASMA APPARATUS OPERATED IN THE RADIOFREQUENCY-SUSTAINED MODE	NASA TN D-7188 ANALYTICAL AND EXPERIMENTAL PERFORMANCE OF OPTIMAL CONTROLLER DESIGNS FOR A SUPERSONIC INLET	NASA TN D-7189 CHEMICAL NONEQUILIBRIUM EFFECTS ON THE INVISCID FLOW IN THE WINDWARD PLANE OF SYMMETRY OF TWO SIMPLIFIED SHUTTLE CONFIGURATIONS	Next

Bound With Nasa Tn D-7180-7185, 7187-7189

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