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INELUENCE OF SUCTION ON SHOCK WAVE-TURBULENT BOUNDARY LAYER INTRACTION FOR TWO-DIMENSIONAL AND AXIALLY SYMMETRIC FLOWS [NASA CR-1639]

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BookSeries: National Aeronautics and Space Adminstration(NASA). Publisher: Washington, D.C. NASA 1970Description: ix,133p.Subject(s): Shock wave-boundary layer interaction | Boundary layer suctionDDC classification: NASA | CR-1639

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1639 (Browse shelf)	Not for loan		TR8213

Total holds: 0

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Previous	NASA CR-1636 POSSIBLE MODIFICATIONS TO THE CALCULATION OF PERCEIVED NOISINESS [NASA CR-1636]	NASA CR-1637 ATTENUATION OF AIRCRAFT NOISE BY WOOD-SIDED AND BRICK-VENEERED FRAME HOUSES [NASA CR- 1637]	NASA CR-1638 - EXPERIMENTAL AND ANALYTICAL INVESTIGATIONS ON MULTIPLE LIQUID IMPACT EROSION [NASA CR- 1638]	NASA CR-1639 INELUENCE OF SUCTION ON SHOCK WAVE-TURBULENT BOUNDARY LAYER INTRACTION FOR TWO-DIMENSIONAL AND AXIALLY SYMMETRIC FLOWS [NASA CR-1639]	NASA CR-1640 A FURTHER STUDY OF JIMSPHERE WIND PROFILES AS RELATED TO SPACE VEHICLE DESIGN AND OPERATIONS[NASA CR-1640]	NASA CR-1901 Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics [NASA CR-1901]	NASA CR-1902 ATTITUDE-REFERENCED RADIOMETER STUDY- Part II- primary calibration System [NASA CR-1902]	Next

Bound With NASA CR-1631-40 (Bound Acc no. 101540)

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