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HYPERSONIC PERFORMANCE OF SEVERAL BASIC AND MODIFIED DIAMOND-CROSS-SECTION DELTA-WING CONFIGURATIONS

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BookPublisher: Nasa, Washington, D.C. 1967Description: 27.DDC classification: NASA | TN D-3894

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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-3894 (Browse shelf)	Not for loan		TR10426

Total holds: 0

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Previous	NASA TN D3880 PLASMA STABILITY AND THE BOHR-VAN LEEUWEN THEOREM.	NASA TN D-3892 CONTRIBUTION OF DOWNSTREAM STATOR TO THE INTERACTION NOISE OF SINGLE-STAGE AXIAL-FLOW COMPRESSOR	NASA TN D-3893 A NUMERICAL METHOD FOR DETERMINING THE AEROELASTIC DIVERGENCE CHARACTERISTICS OF UNGUIDED, SLENDER-BODY, MULTISTAGE LAUNCH VEHICLES	NASA TN D-3894 HYPERSONIC PERFORMANCE OF SEVERAL BASIC AND MODIFIED DIAMOND-CROSS-SECTION DELTA-WING CONFIGURATIONS	NASA TN D-3895 GAS DENISITY MEASUREMENTS USING LIGHT SCATTERING	NASA TN D-3896 EFFECT OF PROPELLANT-FEED-SYSTEM COUPLING AND HYDRAULIC PARAMETERS ON ANALYSIS OF CHUGGING.	NASA TN D-3897 EXPERIMENTAL INVESTIGATION OF INTERFACIAL BEHAVIOR FOLLOWING TERMINATION OF OUTFLOW IN WEIGHTLESSNESS	Next

Bound With Nasa Tn D-3891-93 And D-3895-3900

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