Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests-Reference-Cited by-同舟云学术

Capture Area Ratio and Drag Difference between Wind Tunnel and Flight Tests

Published:2022 Issue:3 Volume:65 Page:134-137
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

YAMADA Kento¹,UCHIYAMA Takahiro¹,UENO Makoto¹

Affiliation:

1. Aviation Technology Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/65/3/65_T-21-18/_pdf

Reference12 articles.

1. 1) Kimzey, W. F., Covert, E. E., Rooney, E. C., Richey, G. K., and James, C. R.: Thrust and Drag: Its Prediction and Verification, American Institute of Aeronautics and Astronautics, Reston, 1985, pp. 173–206.

2. 2) Hoerner, S. F.: Fluid-dynamic Drag, Private Publishing, 1965, pp. 2-1–2-16.

3. 3) Raymer, D. P.: Aircraft Design: a Conceptual Approach, 5th ed., American Institute of Aeronautics and Astronautics, Reston, 2012, pp. 429–438.

4. 4) Webb, L. D., Whitmore, S. A., and Janssen, R. L.: Preliminary Flight and Wind Tunnel Comparisons of the Inlet/Airframe Interaction of the F-15 Airplane, AIAA Paper 79-0102, 1979.

5. 5) Tomita, H. and Naruoka, M.: JAXA Flying Test Bed “Hisho,” Aeronautical and Space Sciences Japan, 62, 6 (2014), pp. 195–201 (in Japanese).

Cited by 2 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. Numerical Study on Variation in Drag Difference by Adding Annular Plug into Flow-Through Nacelle with Integrated Configuration;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2024

2. Flight-to-Wind-Tunnel Correlation Study using JAXA’s Flying Test Bed “Hisho”;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023