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

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1.
NASA Technical Note [NASA TN D-2550]: Application of generalized Newtonian theory to three-dimensional sharp-nose shock-detached bodies at mach for angles of attack up to 25 [degree]

by Washington. National Aeronautics and Space Administration (NASA) | Ashby, George C | Goldberg, Theodore J.

Material type: book Book Description: 41p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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2.
CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UPTO 25(DEGREE)

by Goldberg,Theodore J, Ashby,George C | Hondros,James G.

Material type: book Book Description: 53.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1793 -] (1).

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3.
NASA Technical Note [NASA TN D-2854]: A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a mach number of 6.0

by Washington. National Aeronautics and Space Administration (NASA) | Ashby, George C | Cary, Aubrey M.

Material type: book Book Description: 74p.Publisher: Washington NASA 1965Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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4.
EXPERIMENTAL BOUNDARY-LAYER EDGE MACH NUMBERS FOR TWO SPACE SHUTTLE ORBITERS AT HYPERSONIC SPEEDS.

by Ashby,George C.

Material type: book Book Description: 31.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6574] (1).

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5.
INVESTIGATION OF THE EFFECT OF A GUIDE-VANE-ROTOR COMBINATION ON INLET TOTAL-PRESSURE DISTORTION IN A COMPRESSIBLE FLUID

by Ashby,George C.

Material type: book Book Description: 15.Publisher: Nasa, Washington, D.C. 1959Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-123] (1).

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6.
Effectas of lee surface volume addition on longitudinal aerodynamics of a high lift drag ratio wing body configuration an mach 6.0 [NASA TN D-4361

by Stone David R | Ashby George C.

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

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