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AERODYNAMIC INVESTIGATION OF SHARP CONE-CYLINDER SPIKES ON 120(DEGRE) BLUNTED CONES AT MACH NUMBERS OF 3.00, 4.50, AND 6.00

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BookPublisher: Nasa, Washington, D.C. 1969Description: 39.DDC classification: NASA | TN D-5201

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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-5201 (Browse shelf)	Not for loan		TR13543

Total holds: 0

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Previous	NASA TN D-518 IMPORTANT RESEARCH PROBLEMS IN ADVANCED FLIGHT STRUCTURES DESIGN	NASA TN D-519 AN ANALYSIS OF EXACT AND APPROXIMATE EQUATIONS FOR THE TEMPERATURE DISTRIBUTION IN AN INSULATED THICK SKIN SUBJECTED TO AERODYNAMIC HEATING	NASA TN D-520 OPTIMUM DESIGN OF INSULATED COMPARISION PLATES SUBJECTED TO AERODYNAMIC HEATING	NASA TN D-5201 AERODYNAMIC INVESTIGATION OF SHARP CONE-CYLINDER SPIKES ON 120(DEGRE) BLUNTED CONES AT MACH NUMBERS OF 3.00, 4.50, AND 6.00	NASA TN D-5202 HEAVE RESPONSE OF A PLENUM AIR CUSHION INCLUDING PASSIVE AND ACTIVE CONTROL CONCEPTS	NASA TN D-5203 AN ACCURACY AND SPEED COMPARISON OF THE VINTI AND BROUWER ORBIT PREDICTION METHODS	NASA TN D-5204 PRESSURE DISTRIBUTIONS ON 140(DEGRE),160(DEGRE) AND 180(DEGRE) CONES AT MACH NUMBERS FROM 2.30 TO 4.63 AND ANGLES OF ATTACK FROM 0 (DEGRE) TO 20(DEGRE)	Next

Bound With Nasa Tn D-5200,5202-5210

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