Effectiveness of Film Cooling over Large Angle Blunt Cones in High Speed Carbon Dioxide Flows

Author:

Mohammed Ibrahim S.,Sriram R.,Chattopadhyay S.,Jagadeesh G.,Reddy K. P. J.

Publisher

Springer International Publishing

Reference8 articles.

1. Prasun, N.: Desai and Philip C. Knocke: Mars Exploration Rovers Entry, Descent and Landing Trajectory Analysis, AIAA Paper 2004-5092 (2004)

2. Stewart, D.A., Chen, Y.K.: Hypersonic Convective Heat Transfer over 140-deg Blunt Cones in Different Gases. Journal of Spacecrafts and Rockets 31(5) (1994)

3. Sahooet, N.: al: Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed. Phys. Fluids 17, 36102 (2005)

4. Hepp, A.F., et al.: Chemical Approaches to Carbon Dioxide Utilization for Manned Mars Missions. NASA Technical Memorandum 103728 (1991)

5. Finley, P.J.: The flow of a jet from a body opposing a supersonic free stream. J. Fluid Mech. 26, 337 (1966)

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