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WATER-FILM COOLING OF AN 80(DEGREE) TOTAL-ANGLE CONE AT A MACH NUMBER OF 2 FOR AIRSTREAM TOTAL TEMPERATURES UP TO 3,000(DEGREE)R

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BookPublisher: Nasa, Washington, D.C. 1959Description: 32.DDC classification: NASA | MEMO 12-27-58L -

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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 MEMO 12-27-58L - (Browse shelf)	Not for loan		TR7751

Total holds: 0

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Previous	NASA MEMO 12-2-58W HEAT TRANFER IN THE TURBULENT INCOMPRESSIBLE BOUNDRY LAYER II- STEP WALL-TEMPERATURE DISTRIBUTION.	NASA MEMO 1-22-59A - PRESSURE DISTRIBUTIONS AT TRANSONIC SPEEDS FOR BUMPY AND INDENTED MIDSECTIONS OF A BASIC PARABOLIC-ARC BODY	NASA MEMO 1-22-59L LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES	NASA MEMO 12-27-58L - WATER-FILM COOLING OF AN 80(DEGREE) TOTAL-ANGLE CONE AT A MACH NUMBER OF 2 FOR AIRSTREAM TOTAL TEMPERATURES UP TO 3,000(DEGREE)R	NASA MEMO 12-28-58L - BASIC PRESSURE MEASUREMENTS AT TRANSONIC SPEEDS ON A THIN 45(DEGREE) SWEPTBACK HIGHLY TAPERED WING WITH SYSTEMATIC SPANWISE TWIST VARIATIONS	NASA MEMO 12-30-58L - WEIGHT COMPARISON OF SEVERAL ATTITUDE CONTROLS FOR SATELLITES	NASA MEMO 12-31-58L - FREE-FLIGHT HEAT-TRANSFER INVESTIGATION AT SUPERSONIC SPEEDS OF TWO SLENDER CONE-CYLINDER BODIES AT AN ANGLE OF ATTACK OF 8(DEGREE) WITH ONE BODY ROTATING	Next

Bound With Nasa Memo 12-1-58l-12-31-58l

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