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1. THEORETICAL PRESSURE DISTRIBUTIONS OVER ARBITRARILY SHAPED PERIODIC WAVES IN SUBSONIC COMORESSIBLE FLOW AND COMPARISON WITH EXPERIMENT

by Czarnecki,K. R | Jackson,Mary W.

Material type: book Book Description: 33.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TND-5984 -] (1).

2. EFFECTS OF CONE ANGLE, MACH NUMBER, AND NOSE BLUNTING ON TRANSITION AT SUPERSONIC SPEEDS [NASA TN D-634] : National aeronautics and Space Administration

by Czarnecki, K. R | Jackson, Mary W.

Material type: book Book; Format: print ; Literary form: not fiction Description: 31p.Publisher: Washington, D.C. National aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

3. Investigation by schliern technique of methods of fixing fully turbulent floe on models at supersonic speed [NASA TN D-242]

by Jackson, Mary W. and Czarnecki, K. R | Czarnecki, K. R.

Material type: book Book; Format: print ; Literary form: not fiction Description: 16p.Publisher: Washington, D. C. NASA April 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

4. Measurment by wake momentum surveys at mach 1.61 and 2.01 of turbulent boundary-layer skin friction on five swept wings[NASA TN D3764]

by Sorrells,Russell.B | Jackson,Mary.W | Czarnecki,K.R.

Material type: book Book; Format: print ; Literary form: not fiction Description: 28p.Publisher: Washington,D.C. National Aeronautics And Space Administration 1966Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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