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Wind tunnel measurements of surface pressure fluctuations at mach numbers of 1.6, 2.0 and 2.5 using 12 different trasducers

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BookSeries: National Aeronautics and Space Administration. Publisher: National Aeronautics and Space Administration Washington, D. C. 1972Description: 49p.Subject(s): Transducers

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Reference	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR012259

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Previous	Apollo experience report lunar module structural subsystems	Apollo experience report spacecraft heating environment and thermal protection for a launch through the atmosphere of the earth	Apollo experience report evolution of the attitude time line	Wind tunnel measurements of surface pressure fluctuations at mach numbers of 1.6, 2.0 and 2.5 using 12 different trasducers	Lee surface heating and flow phenomena on shuttle orbiters at large angles of attack and hypersonic speeds	NASA Technical Note [NASA TN D-4442]: Experimental investigation of acoustic liners to suppress screech in storable propellant rocket motors	NASA Technical Note [NASA TN D-4443]: Local afterbody heat transfer to a blunt two-dimensional configuration at mach 8	Next

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