Heat-transfer and ablation-rate correlations for reentry heatshield and nosetip applications
- 17 January 1972
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Carbon-Carbon Materials for Ablative EnvironmentsNuclear Technology, 1971
- Nonsimilar behavior of ablating graphite sphere conesAIAA Journal, 1970
- A Nonsimilar Solution for Multicomponent Reacting Laminar and Turbulent Boundary Layer Flows Including Transverse CurvaturePublished by Defense Technical Information Center (DTIC) ,1970
- EVALUATION OF A TRANSFER COEFFICIENT APPROACH FOR UNEQUAL DIFFUSION COEFFICIENTS.Published by Office of Scientific and Technical Information (OSTI) ,1969
- Nonsimilar solution of the multicomponent laminar boundary layer by an integral-matrix method.AIAA Journal, 1968