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ANALYTICAL AND EXPERIMENTAL EVALUTION OF A TWO-STAGE ANNULAR AIR EJECTOR FOR HIGH ENERGY WIND TUNNELS

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BookPublisher: Nasa, Washington, D.C. 1962Description: 35.DDC classification: NASA | TN D-1215 -

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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-1215 - (Browse shelf)	Not for loan		TR7851

Total holds: 0

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Previous	NASA TN D-1212 - SOME STUDIES OF LIQUID ROTATION AND VORTEXING IN ROCKET PROPELLENT TANKS	NASA TN D-1213 - PERFORMANCE EVALUTION OF A MERCURY-PROPELLANT FEED SYSTEM FOR A FLIGHT-MODEL ION ENGINE	NASA TN D-1214 - INVESTIGATION OF FORCED-CONVECTION NUCLEATE BOILING OF WATER FOR NOZZLE COOLING AT VERY HIGH HEAT FLUXES	NASA TN D-1215 - ANALYTICAL AND EXPERIMENTAL EVALUTION OF A TWO-STAGE ANNULAR AIR EJECTOR FOR HIGH ENERGY WIND TUNNELS	NASA TN D-1216 - STUDY OF A SINUSOIDALLY PERTURBED FLOW IN A LINE INCLUDING A 90(DEGREE) ELBOW WITH FLEXIBLE SUPPORTS	NASA TN D-1218 - MEASUREMENTS OF FLOW DURATION IN A LOW PRESSURE SHOCK TUBE	NASA TN D-1219 - COMPARATIVE MEASUREMENTS OF SINGLY AND DOUBLY IONIZED MERCURY PRODUCED BY ELECTRON BOMBARDMENT ION ENGINE	Next

Bound With Nasa Tn D-1211-20

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