Application of improved k-ω-γ model to deformed hypersonic Inflatable Aerodynamic Decelerator aeroshell

Author:

Zhao Yatian,Chen Jianqiang,Liu Hongkang

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference40 articles.

1. Barton R. Development of Attached Inflatable Decelerators for Supersonic Application[R], NASA CR-66613, 1968.

2. O’Keefe S, Bose D. IRVE-II Post-Flight Trajectory Reconstruction[C]. AIAA Atmospheric Flight Mechanics Conference, Toronto Ontario, 2010.

3. Olds A, Beck R, Bose D, et al. IRVE-3 Post-Flight Reconstruction[C]. AIAA Aerodynamic Decelerator Systems Conference, Daytona Beach Florida, 2013.

4. Corso J, Cheatwood F, Iii W, et al. Advanced High-Temperature Flexible TPS for Inflatable Aerodynamic Decelerators[C]. 21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, Dublin Ireland, 2011.

5. Hughes S, Dillman R, Starr B, et al. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview[C]. 18th Aerodynamic Decelerator Systems Technology Conference and Seminar, Munich Free State of Bavaria, 2005.

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