Measurements of the total surface emittance of charring ablators.
- 1 December 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (12) , 2285-2287
- https://doi.org/10.2514/3.4431
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Prediction of incipient separation in shock- boundary-layer interactions.AIAA Journal, 1967
- Laminar convective heating and ablation in the Mars atmosphere.AIAA Journal, 1967
- Boundary layer separation in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Experimental investigation of a charring ablative material exposed to combined convective and radiative heating.AIAA Journal, 1965
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- THERMAL PERFORMANCE OF HEAT SHIELD COMPOSITES DURING PLANETARY ENTRYPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- THE SPECTRAL EMISSIVITY AND TOTAL NORMAL EMISSIVITY OF COMMERCIAL GRAPHITES AT ELEVATED TEMPERATURESPublished by Elsevier ,1963