Supersonic film cooling-Reference-Cited by-同舟云学术

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Supersonic film cooling

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:2nd International Aerospace Planes Conference
language:
Short-container-title:

Author:

BASS ROBERT¹,HARDIN LARRY¹,RODGERS RICHARD¹,ERNST RICHARD²

Affiliation:

1. United Technologies Research Center, East Hartford, CT

2. Pratt and Whitney Group, West Palm Beach, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-5239

Reference25 articles.

1. M, b c 2* 1.0 3.0 -2.00 0.80 2** 1.0 3.0 -1.20 1.20 3 1.0 6.0 -0.70 0.56 4 2.3 6.0 -0.55 0.44 5t 1.0 6.0 -0.23 0.18

2. 5$ 1.0 6.0 -0.36 0.29 * h<0.12 -

3. M 2 2 CP 3.4 3.4 T, R 2000 530 Relft 3 x lo 6 6 x lo 6 Ttcmtm 0.16 0.14 Descriotion of Wind Tunnel

4. Test Procedure and Data Reduction

Cited by 26 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

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2. Flow structure and cooling effect of seeping gas film in supersonic turbulent boundary layer;Applied Thermal Engineering;2024-07

3. Research progress in aero-optical effects of supersonic turbulent shear layers;Progress in Aerospace Sciences;2024-04

4. Study on the cooling and drag reduction characteristics of multi-port injector array film cooling using gaseous hydrocarbon fuel as coolant;Applied Thermal Engineering;2024-01

5. Research progress of transpiration cooling for aircraft thermal protection;Applied Thermal Engineering;2024-01

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