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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.
EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM..

by Goldberg,Theodore J | Blanchard,Doris K.

Material type: book Book Description: 34.Publisher: Nasa, Washington, D.C. 1963Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-1959 -] (1).

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3.
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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4.
AFTERBODY PRESSURES ON TWO-DIMENSIONAL BOATTAILED BODIES HAVING TURBULENT BOUNDARY LAYERS AT MACH 56.98

by Staylor,W Frank | Goldberg,Theodore J.

Material type: book Book Description: 36.Publisher: Nasa, Washington, D.C. 1964Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-2350] (1).

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5.
HYPERSONIC AERODYNAMIC CHARACTERISTICS OF TWO DELTA-WING X-15 AIRPLANE CONFIGURATIONS

by Goldberg,Theodore J | Hefner,Jerry N.

Material type: book Book Description: 102.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5498] (1).

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6.
INVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION

by Goldberg,Theodore J | Boxer,Emanuel.

Material type: book Book Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).

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