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HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS ON SPHERICALLY BLUNTED 25(DEGREE) HALF-ANGLE CONE AT MACH 8 AND ANGLES OF ATTACK UP TO 90(DEGREE)

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BookPublisher: Nasa, Washington, D.C. 1968Description: 38.DDC classification: NASA | TN D-4792 -

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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-4792 - (Browse shelf)	Not for loan		TR10001

Total holds: 0

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Previous	NASA TN D-4738 INVESTIGATION OF ELECTRON-RADIATION-INDUCED DIELECTRIC BREAKDOWNS IN A TYPICAL CAPACITOR METEOROID DETECTOR SYSTEM	NASA TN D-4739 APPLICATION OF THE LEADING-EDGE-SUCTION ANALOGY OF VORTEX LIFT TO THE DRAG DUE TO LIFT OF SHARP-EDGE DELTA WINGS	NASA TN D-4740 ATTITUDE DETEMINATION OF THE SPIN-STABILIIZED PROJECT SCANNER SPACECRAFT	NASA TN D-4792 - HEAT-TRANSFER AND PRESSURE DISTRIBUTIONS ON SPHERICALLY BLUNTED 25(DEGREE) HALF-ANGLE CONE AT MACH 8 AND ANGLES OF ATTACK UP TO 90(DEGREE)	NASA TN D-4793 - DIVERGENCE OF SOME ALL-MOVABLE CONTROL SURFACES INCLUDING DRAG LOADINGS	NASA TN D-4794 - SURVEY OF CO2 LASER DEVELOPMENT FOR SPACE APPLICATIONS	NASA TN D-4795 - EFFECTS OF BOUNDARY LAYER BUILDUP IN SHOCK TUBES UPON CHEMICAL RATE MEASUREMENTS	Next

Bound With Nasa Tn D-4791-4800

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