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ACCOUSTIC PROPERTIES OF A SUPERSONIC FAN.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 37.DDC classification: NASA | TN D-7096

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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-7096 (Browse shelf)	Not for loan		TR14395

Total holds: 0

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Previous	NASA TN D-7083 APOLLO EXPERIENCE REPORT - LAUNCH ESCAPE PROPULSION SUBSYSTEM	NASA TN D-709 CHOOSING A SUITABLE SWEEP RATE FOR SINUSOIDAL VIBRATION TESTING	NASA TN D-7095 ASYMMERTIC LATERAL-DIRECTIONAL CHRACTERISTICS OF POINTED BODIES OF REVOLUTION AT HIGH ANGLES OF ATTACK.	NASA TN D-7096 ACCOUSTIC PROPERTIES OF A SUPERSONIC FAN.	NASA TN D-7097 NUMERICAL METHOD FOR DESIGN OF MINIMUM-DRAG SUPERSONIC WING CAMBER WITH CONSTRAINTS ON PITCHING MOMENT AND SUFACE DEFORMATION.	NASA TN D-7098 A COMPARISON OF TECHNIQUES FOR INVERSION OF RADIO-RAY DATA IN PRESENCE OF RAY BENDING.	NASA TN D-7099 EFFECT OF WING DESIGN ON THE LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF A WING-BODY.	Next

Bound With Nasa Tn D-7091-7095.7097-7099.Lack No-7094.

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