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PROGRAM AND CHARTS FOR DETERMINING SHOCK TUBE EXPANSION TUBE AND EXPANSION TUNNEL FLOW QUANTITIES FOR REAL AIR

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BookSeries: National Aeronautics And Space Administration Tnd-7752. Publisher: Nasa, Washington, D.C. 1975Description: 278.DDC classification: TR | TND-7752

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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	TR TND-7752 (Browse shelf)	Not for loan		TR2496

Total holds: 0

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Previous	TR TND-7740 SIMULATION STUDIES OF STOL AIRPLANE OPERATIONS IN METROPOLITON DOWNTOWN AND AIRPART AIR TRAFFIC CONTROL ENVIRONMENTS	TR TND-7748 ELASTOPLASTIC ANALYSIS OF A UNIAXIALLY LOADED SHEET WITH AN INTERFERENCE FIT BOLT	TR TND-7749 EXTRACTION FROM FLIGHT DATE OF LATERAL AERODYNAMIC EOFFICIENTS FOR F-8 AIRCRAFT WITH SUPERCRITICAL WING	TR TND-7752 PROGRAM AND CHARTS FOR DETERMINING SHOCK TUBE EXPANSION TUBE AND EXPANSION TUNNEL FLOW QUANTITIES FOR REAL AIR	TR TND-7769 Analytical chemical kinetic investigation of the effects of oxygen,hydrogen,and hydroxyl radicals on hydrogen-air combustion	TR TND-7771 The influence of surface waves on water circulation in a mid-atlantic continental-shelf region	TR TND-7781 Apollo experience report-apollo lunar surface experiments package data processing system	Next

Bound With: Nasa Tnd-7736-7752

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