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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A NONLIFTING VEHICLE SUITABLE FOR REENTRY

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BookPublisher: Nasa, Washington, D.C. 1959Description: 14.DDC classification: NASA | MEMO 4-13-59L -

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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 4-13-59L - (Browse shelf)	Not for loan Untraceable		TR7693

Total holds: 0

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Previous	NASA MEMO 4-11-59L - LOW-SPEED STATIC STABILITY AND CONTROL CHARACTERISTICS OF A MODEL OF A RIGHT TRIANGULAR PYRAMID REENTRY CONFIGURATION	NASA MEMO 4-12-59L - EXPERIMENTAL INVESTIGATION OF EFFECTS OF RANDOM LOADING ON THE FATIGUE LIFE OF NOTCHED CANTILEVER-BEAM SPECIMENS OF 7075-T6 ALUMINUM ALLOY	NASA MEMO 4-13-59E - EXPLORATORY INVESTIGATION OF ADVANCED-TEMPERATURE NICKEL-BASE ALLOYS	NASA MEMO 4-13-59L - WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF A NONLIFTING VEHICLE SUITABLE FOR REENTRY	NASA MEMO 4-14-59E - PRELIMINARY DEVELOPMENT OF ELECTRODES FOR AN ELECTRIC-ARC WIND TUNNEL	NASA MEMO 4-15-59L - CHARTS OF THE INDUCED VELOCITIES NEAR A LIFTING ROTOR	NASA MEMO 4-17-59L - AIRPLANE MEASUREMENTS OF ATMOSPHERIC TURBULENCE AT ALTITUDES BETWEEN 20,000 AND 55,000 FEET FOR FOUR GEOGRAPHIC AREAS	Next

Bound With Nasa Memo 4-1-59l-4-19-59l

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