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LOW-SPEED WIND-TUNNEL INVESTIGATION OF AN ANNULAR-JET CONFIGURATION IN GROUND PROXIMITY

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BookPublisher: Nasa, Washington, D.C. 1963Description: 46.DDC classification: NASA | TN D-1779

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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-1779 (Browse shelf)	Not for loan		TR13163

Total holds: 0

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Previous	NASA TN D-1776 AERODYNAMIC CHARACTERISTICS OF A FLEXIBLE-CANOPY PARAGLIDER MODEL AT A MACH NUMBER OF 4.5 FOR ANGLES OF ATTACK TO 360 DEGREE AND SIDESLIP ANGLES FROM 0 DEGREE TO 90 DEGREE	NASA TN D-1777 AIRCRAFT VORTEX WAKES IN RELATION TO TERMINAL OPERATIONS	NASA TN D-1778 ESTIMATES OF ATTENUATION AND REFLECTION OF TELEMETERING SIGNALS BY IONIZED FLOW FIELDS SURROUNDING TYPICAL REENTRY BODIES	NASA TN D-1779 LOW-SPEED WIND-TUNNEL INVESTIGATION OF AN ANNULAR-JET CONFIGURATION IN GROUND PROXIMITY	NASA TN D-1780 GEOMETRICAL CHARACTERISTICS OF LUNAR ORBITS ESTABILISHED FROM EARTH-MOON TRAJECTORIES	NASA TN D-1782 - SIMPLIFIED METHOD FOR MEASURING HUMAN TRANSFER FUNCTION	NASA TN D-1793 - CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UPTO 25(DEGREE)	Next

Bound With Nasa Tn D-1771-78,1780

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