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Research on thermal protection by opposing jet and transpiration for high speed vehicle

  • Published:2016-01 Issue: Volume:48 Page:322-327
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Rong Yisheng,Wei Yuechuan,Zhan Renjun

Funder

Natural Science Foundation Project of Shaanxi Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Hypersonic vehicle thermal structure test challenges;Swanson,2007

2. A review of hypersonics aerodynamics, aerothermodynamics and plasmadynamics activities within NASA's fundamental aeronautics program;Salas,2007

3. Calibration of thermal paints for hypersonic flight test;Neely,2008

4. Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles;Glass,2008

5. Transpiration cooling using liquid water;Van Foreest,2007

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1. Tolerance indicating models of non-thermal and thermal damages for a heat transport system;International Journal of Heat and Mass Transfer;2024-06

2. Fundamentals and recent progress of additive manufacturing-assisted porous materials on transpiration cooling;Journal of the Global Power and Propulsion Society;2023-07-27

3. Phenomenological Introduction of Standoff Distance of Sonic Ring Impelling Entropy Waves and Aerodynamic Heating of Hypersonic Vehicles;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

4. Fluidic techniques;Aerodynamic Heating in Supersonic and Hypersonic Flows;2023

5. Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet;Journal of Aerospace Engineering;2022-09
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