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COMPARISONS OF TWO-DIMENSIONAL SHOCK-EXPANSION THEORY WITH EXPERIMENTAL AERODYNAMIC DATA FOR DELTA-PLANFORM WINGS AT HIGH SUPERSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1974Description: 36.DDC classification: NASA | TN D-7583 -

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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-7583 - (Browse shelf)	Not for loan		TR10058

Total holds: 0

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Previous	NASA TN D-758 - HEAT-TRANSFER TESTS OF 20-MILLIMETER PROJECTILES AT A MACH NUMBER OF 5 WITH AN ANALYSIS BY UNSTEADY SCALING LAWS TO PREDICT COMPONENT TEMPERATURE RISES AFTER FIRING FOR VARIOUS FREE -FLIGHT CONDITIONS	NASA TN D-7580 - ALGORITHM FOR A GENERAL CLASS OF ROUTINE PROBLEMS DERIVED FROM HUYGENS' PRINCIPLE	NASA TN D-7582 - SYSTEM FOR SPACECRAFT ATTITUDE CONTROL AND ENERGY STORAGE	NASA TN D-7583 - COMPARISONS OF TWO-DIMENSIONAL SHOCK-EXPANSION THEORY WITH EXPERIMENTAL AERODYNAMIC DATA FOR DELTA-PLANFORM WINGS AT HIGH SUPERSONIC SPEEDS	NASA TN D-7584 - HEAT TRANSFER CHARACTERISTICS OF AN EMERGENT STRAND	NASA TN D-7585 - APOLLO EXPERIENCE REPORT-COMMAND AND SERVICE MODULE COMMUNICATIONS SUBSYSTEM	NASA TN D-7586 - APOLLO EXPERIENCE REPORT-PROBLEM REPORTING AND CORRECTIVE ACTION SYSTEM	Next

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