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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

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BookPublisher: Nasa, Washington, D.C. 1974Description: 299.DDC classification: NASA | CR-2436 -

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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-2436 - (Browse shelf)	Not for loan		TR8662

Total holds: 0

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Previous	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]	NASA CR-2442 Prediction of sonic boom from experimental near-field overpressure data. Volume 2: Data base construction[NASA CR-2442]	NASA CR-2444 Analysis of pilot error-related aircraft accidents [NASA CR-2444]	Next

Bound With Nasa Cr-2431-40

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