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Flow-field measurement of two protuberances on a flat plate submerged in a turbulent boundary layer at mach 2.49 and 4.44 [NASA TN D-5297]

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Material type: Text

TextLanguage: English Series: National Aeronautics and Space Administration (NASA)Publication details: NASA 1969 Washington, D.C.Description: 135pSubject(s):

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NASA technical note D-5297

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Holdings
Item type	Current library	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		Not for loan		TR14385 [D-5297]

Total holds: 0

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Previous	Fatigue of notched Ti-8Al-1mo-1V titanium alloy at room temperature and 55o degree F (560 degree K) with Flight by flight loading representative of a supersonic transport [NASA TN D-5294]	Description of high enthalpy arc tunnel at the langley research center including test-stream conditions at selected operating points [NASA TN D-5295]	Inflation and performance of three parachute configurations from supersonic flight tests in a low-density environment [D5296]	Flow-field measurement of two protuberances on a flat plate submerged in a turbulent boundary layer at mach 2.49 and 4.44 [NASA TN D-5297]	Flight investigation of a fluidic autopilot system [NASA TN D-5298]	Evaluation of an indirect viewing system for lifting body thermal -area navigation and landing tasks [NASA TN D-5299]	LONGITUDINAL OSCILLATION OF LAUNCH VEHICLES.	Next

NASA technical note D-5297

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