Shape Change and Conduction for Nosetips at Angle of Attack
- 1 May 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (5) , 599-604
- https://doi.org/10.2514/3.49771
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Three-dimensional nosetip shape changes in hypersonic flow. I - Illustration of a mathematical model-characteristic methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Transitional and Turbulent Heat-Transfer Measurements on a Yawed Blunt Conical NosetipAIAA Journal, 1972
- Low temperature ablator nosetip shape change at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Heat-transfer correlations for blunt cones at angle of attackJournal of Spacecraft and Rockets, 1971
- Turbulent HeatmTransfer Measurements on a Blunt Cone at Angle of AttackAIAA Journal, 1971
- Axisymmetric ablation with shape changes and internal heat conductionAIAA Journal, 1970
- Surface geometry of three-dimensional inviscid hypersonic flows.AIAA Journal, 1969
- The Solution of Heat Conduction Problems by Probability MethodsJournal of Heat Transfer, 1967