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COMPRESSIBLE TURBULENT BOUNDARY LAYER ON ABLUNT SWEPT SLAB WITH AND WITHOUT LEADING-EDGE BLOWING

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BookPublisher: Nasa, Washington, D.C. 1971Description: 61.DDC classification: NASA | TN D-6203 -

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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-6203 - (Browse shelf)	Not for loan		TR10380

Total holds: 0

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Previous	NASA TN D-620 - Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30(degree) sweptback wing at transonic speeds	NASA TN D-6201 - WIND-TUNNEL INVESTIGATION OF SONIC-BOOM CHARACTERISTICS OF TWO SIMPLE WING MODELS AT MACH NUMBERS FROM 2.3 TO 4.63	NASA TN D-6202 - EXPERIMENTAL INVESTIGATION OF THE DIRECTIONAL CONTROL CAPABILITY OF 18 X 5.5,TYPE VII,AIRCRAFT TIRES ON WET SURFACES	NASA TN D-6203 - COMPRESSIBLE TURBULENT BOUNDARY LAYER ON ABLUNT SWEPT SLAB WITH AND WITHOUT LEADING-EDGE BLOWING	NASA TN D-6204 - CLOSED-LOOP IONOGRAM PROCESSOR FOR THE ANALYSIS OF TOPSIDE SOUNDER IONOGRAM FILMS (FILMCLIP)	NASA TN D-6205 - EXPERIMENTAL INVESTIGATION OF THE AIRLOW OVER A CAVITY WITH ANTIRESONANCE DEVICES	NASA TN D-6206 - PROBABILITY CONCEPTS APPLIED TO SEQUENTIAL EQUIPMENT OPERATION	Next

Bound With Nasa Tn D-6200-19

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