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Vortex flow and erosion on rocket nozzles due to warm-gas injection for thrust vector control[NASA TN D-3242]

By: Smith, G. Louis.

Series: National Aeronautics and Space Adminstration ; NASA technical note. Publisher: Washington,D.C. Natoonal Aeronautics and Space Adminstartion 1966Description: 23p.Subject(s): Rocket nozzles

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D 3241-3250	Not for loan		TR64307

Total holds: 0

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Previous	A use of conformal mapping to determine the apparent additional mass of scalloped and/or clustered cylinder configurations with experimental evaluations of results[NASA TN D-1373]	Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ratio wings having variations in leading-edge contour[NASA TN D-1374]	An investigation of periodic forces and moments transmitted to the hub of four lifting rotor configurations [NASA TN D-1011]	Vortex flow and erosion on rocket nozzles due to warm-gas injection for thrust vector control[NASA TN D-3242]	The determiniation of a stability indicative function for linear systems with mutiple delays [NASA TR R-301]	Use of superposition in digital computers to obtain wind tunnel interference factors for arbitrary configurations with particular reference to V/Stol models [NASA TR R-302]	Causes of magnetic field nonuniformity and its effect on stability of theta pinch plasma [NASA TR R-303]	Next

Bound vol. contains D 3241-3250

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