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1. Neasurement of aerodynamics heat transfer to a deflected trailing edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6

by Chauvin, Leo T. and Buglia James J | Buglia James J.

Material type: book Book; Format: print ; Literary form: not fiction Description: 18p.Publisher: Washington, D. C. NASA June 1960Availability: No items available

2. Neasurement of aerodynamics heat transfer to a deflected trailing edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6 [NASA Tn D-250]

by Chauvin, Leo T. and Buglia James J | Buglia James J.

Material type: book Book; Format: print ; Literary form: not fiction Description: 18p.Publisher: Washington, D. C. NASA June 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

3. Measurements of aerodynamic heat transfer and boundary-layer transition on a 15 deg. cone in free flight at supersonic mach numbers up to 5.2 [NASA TN D-888]

by Rumsey, Charles B | Lee, Dorothy B.

Material type: book Book; Format: print ; Literary form: not fiction Description: 43p.Publisher: Nasa Washington 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-888] (1).

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