Investigation of heat transfer mechanism of low environmental pressure large-space spray cooling for near-space flight systems-Reference-Cited by-同舟云学术

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Investigation of heat transfer mechanism of low environmental pressure large-space spray cooling for near-space flight systems

Published:2018-04 Issue: Volume:119 Page:496-507
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Wang Ji-Xiang,Li Yun-Ze,Yu Xi-Kui,Li Guang-Chao,Ji Xin-Yan

Funder

Shenyang Aircraft Design and Research Institute

Young Scientist Training Program of National Laboratory for Aeronautics and Astronautics

Academic Excellence Foundation

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference36 articles.

1. Adaptive neural prescribed performance tracking control for near space vehicles with input nonlinearity;Yang;Neurocomputing,2016

2. Robust attitude control of near space vehicles with time-varying disturbances;Chen;Int. J. Control Autom. Syst.,2013

3. T. Kojima, H. Taguchi, S. Imamura, H. Kobayashi et al., Conceptual study on heat resistant and cooling system of hypersonic airplane, in: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Apr. 11–14, 2011.

4. Near-space station-keeping performance of a large high-altitude notional airship;Schmidt;J. Aircraft,2007

5. A highly self-Adaptive cold plate for the single-phase mechanically Pumped Fluid Loop for Spacecraft Thermal Management;Wang;Energy Convers. Manage.,2016

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