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A METHOD FOR CALCULATING AERODYNAMICS LOADING ON THE WINGS AT A MACH NUMBER OF 1.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 96.DDC classification: NASA | TN D-96

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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-96 (Browse shelf)	Not for loan		TR15737

Total holds: 0

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Previous	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)	NASA TN D-963 PAYLOAD VIBRATION DATA MEASURED DURING FIVE FLIGHTS OF A TWO-STAGE SOLID-PROPELLANT LAUNCH VEHICLE	NASA TN D-964 THE USE OF HIGHER-ORDER DIFFERENCE METHODS IN BEAM VIBRATION ANALYSIS	Next

Bound With Nasa Tn D-91-95,97-100.

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