Welcome to P K Kelkar Library, Online Public Access Catalogue (OPAC)

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1. A SEMIGRAPHICAL METHOD OF APPLYING IMPACT THEORY TO AN ARBITRARY BODY TO OBTAIN THE HYPERSONIC AERODYNAMIC CHARACTERISTICS AT ANGLE OF ATTACK AND SIDESLIP [NASA TN D-795]

by Jackson, Charlie M.

Material type: book Book; Format: print ; Literary form: not fiction Description: 18p.Publisher: Washington, D.C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

2. A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570]

by Wilbur, D. Middleton | Carlson, Harry W.

Material type: book Book; Format: print ; Literary form: not fiction Description: 23p.Publisher: Washington, D. C NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2570] (1).

3. General potential theory of arbitrary wing sections [Report no. 452]

by Theodorsen, T | Garrick, I. E.

Material type: book Book; Format: print ; Literary form: not fiction Description: 35p.Publisher: Washington, D. C. National Advisory Committee for Aeronautics 1940Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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