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1. EFFECTS OF ANGLE OF ATTACK AND BLUNTNESS ON THE HYPERSONIC FLOW OVER A 15 (DEGRE) SEMIAPEX CONE IN HELIUM

by Cleary,Joseph W | Duller,Charles E.

Material type: book Book Description: 40.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5903] (1).

2. NASA Technical Note [NASA TN D-4909]: Effects of angle of attack and bluntness on the shock-layer properties of a 15 degree cone at a mach number of 10.6

by Washington. National Aeronautics and Space Administration (NASA) | Cleary, Joseph W.

Material type: book Book Description: 38p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

3. APPROXIMATION FOR DISTRIBUTION OF FLOW PROPERTIES IN THE ANGLE-OF-ATTACK PLANE OF CONICAL FLOWS

by Cleary,Joseph W.

Material type: book Book Description: 22.Publisher: Nasa, Washington, D.C. 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5951] (1).

4. EFFECTS OF ANGLE OF ATTACK AND BLUNTNESS ON LAMINAR HEATING-RATE DISTRIBUTIONS OF A 15 DEGREE CONE AT A MACH NUMBER OF 10.6

by Cleary,Joseph W.

Material type: book Book Description: 53.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5450] (1).

5. Theoretical aerodynamic characteristics of sharp and

by Cleary,Joseph W.

Material type: book Book; Format: print ; Literary form: not fiction Availability: No items available

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