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THEORETICAL AND EXPERIMENTAL LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF AN ASPECT RATIO 0.25 SHARP-EDGE DELTA WING AT SUBSONIC, SUPERSONIC,AND HYPERSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1974Description: 69.DDC classification: NASA | TN D-7651

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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-7651 (Browse shelf)	Not for loan		TR11641

Total holds: 0

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Previous	NASA TN D-7649 INTERFERENCE HEATING FROM INTERACTIONS OF SHOCK WAVES WITH TURBULENT BOUNDARY LAYERS AT MACH 6	NASA TN D-765 EXPERIMENTAL HEAT TRANSFER AND PRESSURE DROP OF LIQUID HYDROGEN FLOWING THROUGH A HEATED TUBE	NASA TN D-7650 AERODYNAMIC AND FLOW-VISUALIZATION STUDIES OF VARIATIONS IN THE GEOMETRY OF IRREGULAR PLANFORM WINGS AT A MACH NUMBER OF 20.3.	NASA TN D-7651 THEORETICAL AND EXPERIMENTAL LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF AN ASPECT RATIO 0.25 SHARP-EDGE DELTA WING AT SUBSONIC, SUPERSONIC,AND HYPERSONIC SPEEDS	NASA TN D-7652 PARAMETRIC ANALYSIS OF AN IMAGING RADAR FOR USE AS AN INDEPENDENT LANDING MONITOR	NASA TN D-7653 CALCULATION OF SUPERSONIC STREAM PARAMETERS OF A REAL GAS FROM MEASURABLE QUANTITIES USING FORTRAN IV ROUTINES	NASA TN D-7654 EFFECTS ON SIGMA-PHASE FORMATION ON SOME MECHANICAL PROPERTIES OF A WROUGHT NICKEL-BASE SUPERALLOY(IN-100)	Next

Bound With Nasa Tn D-7648-50, 7652-60.

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