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INVESTIGATION OF HIGH-SPEED IMPACT : REGIONS OF IMPACT AND IMPACT AT OBLIQUE ANGLES.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 18.DDC classification: NASA | TN D-94

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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-94 (Browse shelf)	Not for loan		TR15735

Total holds: 0

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Previous	NASA TN D-93 APPLICATIOIN TO FLUID DYNAMIC OF THE THEORY OF REVERSIBLE HEAT ADDITION.	NASA TN D-930 - LINEAR THEORY FOR INFLATABLE PLATES OF ARBITRARY SHAPE	NASA TN D-9306 - USE OF TUNGSTEN-184 AS A THERMAL FLUX MONITOR AT HIGH TEMPERATURES	NASA TN D-94 INVESTIGATION OF HIGH-SPEED IMPACT	NASA TN D-95 THEORETICAL ANALYSIS OF THE CREEP COLLAPSE OF COLUMNS.	NASA TN D-96 A METHOD FOR CALCULATING AERODYNAMICS LOADING ON THE WINGS AT A MACH NUMBER OF 1.	NASA TN D-962 LAMINAR HEAT-TRANSFER AND PRESSURE MEASUREMENTS AT A MACH NUMBER OF 6 ON SHARP AND BLUNT 15 (DEGREE) HALF-ANGLE CONES AT ANGLES OF ATTACK UP TO 90(DEGREE)	Next

Bound With Nasa Tn D-91-93,95-100.

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