Mathematical Modeling of Aerodynamic Heating and Pressure Distribution on a 5-Inch Hemispherical Concave Nose in Supersonic Flow

Author:

P. Spiridakos Dimitrios,C. Markatos Nicholas,Karadimou Despoina

Publisher

IntechOpen

Reference13 articles.

1. Thompson J, Birk AM, Cunningham M. Design of infrared signature suppressor for the bell 205 (UH-1H) helicopters, part 1: Aerothermal design. In: Seventh CASI Propulsion Symposium. 1999

2. Riley CJ, DeJarnette FR. An Engineering Aerodynamic Heating Method for Hypersonic Flow. American Institute of Aeronautics and Astronautics; 1992

3. PHOENICS. VR Reference Guide: Documentation for Phoenics (TR 326), Version 2010. London, UK: CHAM; 2010

4. Rooks S. Preliminary Investigations into the Use of PHOENICS for Evaluation of Aerodynamic Heating Phenomena. DRA Farnborough; 1996

5. Murakami K, Yamamoto Y, Rouzand O. CFD Analysis of Aerodynamic Heating for HYFLEX High Enthalpy Flow Tests and Flight Conditions. 24th International Congress of the Aeronautical Sciences; 2004

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