Navier–Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles-Reference-Cited by-同舟云学术

Navier–Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles

Published:2006-07 Issue:5 Volume:10 Page:374-384
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cayzac Roxan,Grignon Christophe,Carette Eric

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. B.S. Baldwin, H. Lomax, Thin layer approximation and algebraic model for separated turbulent flows, AIAA Paper 78-257, January 1978

2. M. Péchier, Numerical predictions of magnus effects over ammunition configurations, Ph.D. Dissertation, Mechanical Engineering, University of Poitiers, Poitiers, France, September 1999 (in French)

3. Magnus effect over finned projectiles;Péchier;J. Spacecraft and Rockets,2002

4. Approximate Rieman solvers, parameter vectors and difference schemes;Roe;J. Comput. Phys.,1981

5. Towards the ultimate conservative differencing scheme II: Monotonicity and conservation combined in a second order scheme;Van Leer;J. Comput. Phys.,1974

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Research on the cooling performance of the discontinuous transpiration surface structure for the leading edge of a hypersonic vehicle;Applied Thermal Engineering;2024-03

2. Evaluation of high-speed aircraft thermal management system based on spray cooling technology: Energy analysis, global cooling, and multi-objective optimization;Applied Thermal Engineering;2023-07

3. Ablation Behavior of Rudder Wing Structure in Hypersonic Environment;Journal of Aerospace Engineering;2023-07

4. Rapid Steady-State Hypersonic Aerothermodynamic Loads Prediction Using Reduced Fidelity Models;Journal of Aircraft;2021-05

5. Multidisciplinary Shape Optimization of Missile Fin Configuration Subject to Aerodynamic Heating;Journal of Spacecraft and Rockets;2020-05