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Aerodynamic intraction effects ahead of a sonic jet exhausting perpendiculary from a flat plate in to a mach number 6 free stream

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BookPublisher: Washington D. C. NASA 1961Description: 26p.Subject(s): AerodynamicDDC classification: NASA | TN D-743

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-743 (Browse shelf)	Not for loan		TR11866

Total holds: 0

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Previous	NASA TN D-7400 PERFORMANCE ANALYSIS OF THE ASCENT PROPULSION SYSTEM OF THE APOLLO SPACECRAFT	NASA TN D-741 A theoretical analysis of effects of ablation on heat transfer to an arbitrary axisymmetric body [NASA TN D - 741--TN D-750]	NASA TN D-742 Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter	NASA TN D-743 Aerodynamic intraction effects ahead of a sonic jet exhausting perpendiculary from a flat plate in to a mach number 6 free stream	NASA TN D-744 Airspeed operating practices of turbine-powered commercial transport airplanes	NASA TN D-7440 APOLLO EXPERIENCE REPORT COMMAND MODULE CREW-COUCH/RESTRAINT AND LOAD-ATTENUATION SYSTEMS	NASA TN D-745 Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9	Next

Bound With NASA TN D-741-750

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