Heat-Transfer Measurements on Hemispheres in Hypersonic Flight through Air and CO2

Author:

Wilder Michael1,Reda Daniel1,Prabhu Dinesh2

Affiliation:

1. NASA Ames Research Center

2. ERC, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. 1Strawa, A. W., Chapman, G. T., Canning, T. N., and Arnold, J. O. "The Ballistic Range and Aerotherhodynamic Testing," AIAA88-2015,15th AerodynamicTestingConference, San Diego, CA, May18-20, 1988.

2. 2Yee, L.,Bailey, H.E.,andWoodward,H.T."BallisticRangeMeasurementsofStagnation-PointHeatTransferin Airandin Carbon DioxideatVelocitiesupto 18,000FeetPer Second,"NASA TND-777, March1961.

3. 3Dale L. Compton and David M. Cooper, "Free-Flight Measurements of Stagnation-Point Convective Heat Transfer at Velocitiesto41,000 ft/sec,"NASA TND-2871,June1965.

4. Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range

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