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EXHAUST JET WAKE AND THRUST CHARACTERISTICS OF SEVERAL NOZZLES DESIGNED FOR VTOL DOWNWASH SUPPRESSION

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BookPublisher: Nasa, Washington, D.C. 1966Description: 97.DDC classification: NASA | CR-373 -

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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 CR-373 - (Browse shelf)	Not for loan		TR8930

Total holds: 0

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Previous	NASA CR-37 - FINITE ELEMENT SOLUTION FOR THIN SHELLS OF REVOLUTION	NASA CR-370 AN ACOUSTICAL STUDY OF THE KIWI B NUCLEAR ROCKET.	NASA CR-372 - APPLICATION OF WEDGE DIFFRACTION TO ANTENNA THEORY	NASA CR-373 - EXHAUST JET WAKE AND THRUST CHARACTERISTICS OF SEVERAL NOZZLES DESIGNED FOR VTOL DOWNWASH SUPPRESSION	NASA CR-374 - FINAL REPORT FOR A BRUSHLESS D. C. TORQUE MOTOR	NASA CR-375 - SOME STUDIES OF NONLINEAR LATERAL SLOSHING IN RIGID CONTAINERS	NASA CR-376 - PRELIMINARYSTUDY OF CERTAIN ELECTRICAL PROPERTIES OF STANNIC OXIDE CERAMICS	Next

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