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EXPERIMENTAL LOW-SPEED AND CALCULATED HIGH-SPEED AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC RESEARCH AIRPLANE CONCEPT HAVEING A 65DEGREE SWEPT DELTA WING.

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BookPublisher: Nasa, Washington, D.C. 1974Description: 71.DDC classification: NASA | TN D-7633

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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-7633 (Browse shelf)	Not for loan		TR12542

Total holds: 0

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Previous	NASA TN D-763 INTERNAL-PERFORMANCE EVALUATION OF TWO FIXED-DIVERGENT-SHROUD EJECTORS	NASA TN D-7630 - SUBSONIC ANNULAR WING THEORY WITH APPLICATION TO FLOW ABOUT NACELLES	NASA TN D-7632 HOLOGRAPHIC AND ULTRASONIC DETECTION OF BOND FLAWS IN ALUMINUM PANELS REINFORCED WITH BORON-EPOXY.	NASA TN D-7633 EXPERIMENTAL LOW-SPEED AND CALCULATED HIGH-SPEED AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC RESEARCH AIRPLANE CONCEPT HAVEING A 65DEGREE SWEPT DELTA WING.	NASA TN D-7634 DIFFUSION WITH CHEMICAL REACTION	NASA TN D-7635 DIFFERENTIAL ANALYSIS FOR THE TURBULENT BOUNDARY LAYER ON A COMPRESSOR BLADE ELENMENT (INCLUDING BOUNDARY-LAYYER SEPARATION)	NASA TN D-7636 EFFECT OF GEOMETRICAL AND FLOW PARAMETERS ON HIGH-EFFECTIVENESS REGION OF FILM COOLING.	Next

Bound With Nasa Tn D-7631-32,7633-40

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