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ACOUSTIC RADAR INVESTIGATION OF BOUNDARY LAYER PHENOMENA

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BookPublisher: Nasa, Washington, D.C. 1974Description: 65.DDC classification: NASA | CR-2432 -

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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 CR-2432 - (Browse shelf)	Not for loan		TR8658

Total holds: 0

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Previous	NASA CR-2381 An experimental study of the validity of the heat-field concept for sonic-boom alleviation [NASA CR-2381]	NASA CR-2382 - Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures [NASA TN D-2382]	NASA CR-2383 - , Washington, D.C./attitude control system(ipacs) study [NASA CR-2383]	NASA CR-2432 - ACOUSTIC RADAR INVESTIGATION OF BOUNDARY LAYER PHENOMENA	NASA CR-2435 - LATERAL CONDUCTION EFFECTS ON HEAT-TRANSFER DATA OBTAINED WITH THE PHASE-CHANGE PAINT TECHNIQUE	NASA CR-2436 - REDUCTION OF ACOUSTIC DISTURBANCES IN THE TEST SECTION OF SUPERSONIC WIND TUNNELS BY LAMINARIZING THEIR NOZZLE AND TEST SECTION WALL BOUNDARY LAYERS BY MEANS OF SUCTION	NASA CR-2441 Prediction of sonic boom from experimental near-field overpressure data. Volume 1: Method and results[NASA CR-2441]	Next

Bound With Nasa Cr-2431-40

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