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COMPARISON OF WIND-TUNNEL AND FLIGHT MEASURED BASE PRESSURES FROM THE SHARP-LEADING-EDGE UPPER VERTICAL FIN OF THE X-15 AIRPLANE FOR TURBULENT FLOW AT MACH NUMBERS FROM 1.5 TO 5.0

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BookSeries: National Aeronautics And Space Administration Tnd-6348. Publisher: Nasa, Washington, D.C. 1971Description: 38.DDC classification: TR | TND-6348

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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-6348 (Browse shelf)	Not for loan		TR2418

Total holds: 0

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Previous	TR TND-1100 Design of various types of air bearngs for simulating frictionless environments	TR TND-6346 EFFECTS OF SPANWISE VARIATION OF GUST VELOCITY ON ALLEVIATION SYSTEM DESIGNED FOR UNIFORM GUST VELOCITY ACROSS SPAN	TR TND-6347 Goodard research and engineering management exercise	TR TND-6348 COMPARISON OF WIND-TUNNEL AND FLIGHT MEASURED BASE PRESSURES FROM THE SHARP-LEADING-EDGE UPPER VERTICAL FIN OF THE X-15 AIRPLANE FOR TURBULENT FLOW AT MACH NUMBERS FROM 1.5 TO 5.0	TR TND-6349 FUNDAMENTAL TECHNIQUES OF WEIGHT ESTIMATING AND FORECASTING FOR ADVANCED MANNED SPACECRAFT AND SPACE STATIONS	TR TND-6777 FLIGHT-DETERMINED DERIVATIVES AND DYNAMIC CHARACTERISTICS OF THE CV-990 AIRPLANE	TR TND-7729 A Study of the possible charteritics of a low-altitude electron layer in the martian atmosphere	Next

Bound With: Nasa Tnd-6346-49

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