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SHOCK-TUBE FLOW ANALYSIS WITH A DIMENSIONLESS VELOCITY NUMBER

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BookPublisher: Nasa, Washington, D.C. 1969Description: 17.DDC classification: NASA | TN D-5518

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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-5518 (Browse shelf)	Not for loan		TR15206

Total holds: 0

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Previous	NASA TN D-5515 THE EFFECT OF OBJECT MOTION IN FRAUNHOFER HOLOGRAPHY WITH APPLICATION TO VELOCITY MEASUREMENTS	NASA TN D-5516 A METHOD FOR SOLVING THE NONSIMILAR LAMINAR BOUNDARY-LAYER EQUATIONS INCLUDING FOREIGN GAS INJECTION	NASA TN D-5517 FLOWMETER FOR SPACE	NASA TN D-5518 SHOCK-TUBE FLOW ANALYSIS WITH A DIMENSIONLESS VELOCITY NUMBER	NASA TN D-5521 EFFECTS OF BIAS LIGHT AND HEAT TREATMENT ON THE SPECTRAL RESPONSE OF CADMIUM SULFIDE THIN FILM PHOTOVOLTAIC CELLS	NASA TN D-5523 BOUNDARY-LAYER VELOCITY PROFILES DOWNSTREAM OF THREE-DIMENSIONAL TRANSITION TRIPS ON A FLAT PLATE AT MACH 3 AND 4.	NASA TN D-5524 EXPERIMENTAL INVESTIGATION OF ALUMINIDE-COATED TA-10W FOR HEAT-SHELD APPLICATIONS.	Next

Bound With Nasa Tn D-5510-17

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