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IMPORTANT RESEARCH PROBLEMS IN ADVANCED FLIGHT STRUCTURES DESIGN

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BookPublisher: Nasa, Washington, D.C. 1960Description: 49.DDC classification: NASA | TN D-518

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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-518 (Browse shelf)	Not for loan		TR15766

Total holds: 0

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Previous	NASA TN D-5168 VARIATION OF CONVECTIVE HEART-TRANSFER COEFFICIENT AROUND A SIMULATED ROCKET COOLING TUBE SECTION.	NASA TN D-517 NEAR-FIELD AND FAR-FIELD NOISE MEASUREMENTS FOR A BLOWDOWN-WIND-TUNNEL SUPERSONIC EXHAUST JET HAVING ABOUT 475,000 POUNDS OF THRUST	NASA TN D-5170 SHAFT FACE WITH SELF-ACTING LIFT AUGMENTATION FOR ADVANCED GAS TURBINE ENGINES.	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	Next

Bound With Nasa Tn D-511-17,519-20

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