Experimental Investigation on Infrared Radiation Characteristics of Two-Dimensional Convergent–Divergent Vectoring Nozzle-Reference-Cited by-同舟云学术

Experimental Investigation on Infrared Radiation Characteristics of Two-Dimensional Convergent–Divergent Vectoring Nozzle

Published:2019-07 Issue:3 Volume:33 Page:627-637
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Wang Hao¹,Ji Honghu¹,Lu Haohao²

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 20016 Nanjing, People’s Republic of China

2. Aero Engine Corporation of China, 110015 Shenyang, People’s Republic of China

Funder

Fundamental Research Funds for the Central Universities

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.T5592

Reference23 articles.

1. Initial flight test evaluation of the F-15 active axisymmetric vectoring nozzle performance

2. BurchanF. W.RayR. R.ConnersT. R.WalshK. R. “Propulsion Flight Research at NASA Dryden from 1967 to 1997,” NASA TP-206554, 1998. doi:10.2514/6.1998-3712

3. MercerC. E.BerrierB. L. “Effect of Afterbody Shape, Nozzle Type, and Engine Lateral Spacing of the Installed Performance of a Twin-Jet Afterbody Model,” NASA TM X-1855, 1969.

4. F-15 Nozzle/Afterbody Integration

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