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EXPERIMENTAL INVESTIGATION OF AIR FILM COOLING APPLIED TO AN ADIABATIC WALL BY MEANS OF AN AXIALLY DISCHARGING SLOT

By: Papell,S Stephen.

Contributor(s): Trout,Arthur M.

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BookPublisher: Description: 63.DDC classification: NASA | TN D-9

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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-9 (Browse shelf)	Not for loan		TR15302

Total holds: 0

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Previous	NASA TN D-897 EXPLORATORY ENVIRONMENTAL TESTS OF SEVERAL HEAT SHIELDS	NASA TN D-898 REPEATABILITY OF THE OVER-ALL ERRORS OF AN AIRPLANE ALTIMETER INSTALLATION IN LANDING-APPROACH OPERATIONS	NASA TN D-899 AN INVESTIGATION OF LANDING-CONTACT CONDITIONS FOR TWO LARGE TURBOJET TRANSPORTS AND A TURBOPROP TRANSPORT DURING ROUTINE DAYLIGHT OPERATIONS	NASA TN D-9 EXPERIMENTAL INVESTIGATION OF AIR FILM COOLING APPLIED TO AN ADIABATIC WALL BY MEANS OF AN AXIALLY DISCHARGING SLOT	NASA TN D-900 AERODYNAMIC LOAD MEASUREMENTS AND OPENING CHARACTERISTICS OF AUTOMATIC LEADING-EDGE SLATS ON A 45(DEGREE) SWEPTBACK WING AT TRANSONIC SPEEDS	NASA TN D-902 - APPLICATIONS OF POWER SPECTRAL ANALYSIS METHODS TO MANEUVER LOADS OBTAINED ON JET FIGHTER AIRPLANES DURING SERVICE OPERATIONS	NASA TN D-903 - EFFECT AT HIGH SUBSONIC SPEEDS OF FUSELAGE FOREBODY STRAKES ON THE STATIC STABILITY AND VERTICAL-TAIL-LOAD CHARACTERISTICS OF A COMPLETE MODEL HAVING A DELTA WING	Next

Bound With Nasa Tn D-1-7,10 Lack No.8

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