Factors affecting phase-change paint heat-transfer data reduction with emphasis on wall temperatures approaching adiabatic conditions
- 16 August 1972
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A method of solving the three-dimensional laminar boundary-layer equations with application to a lifting re-entry body.AIAA Journal, 1968
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949