Aerodynamic Characteristics of a Slender-Body Ejecting a Supersonic Jet-Reference-Cited by-同舟云学术

Aerodynamic Characteristics of a Slender-Body Ejecting a Supersonic Jet

Published:2022 Issue:0 Volume:20 Page:59-63
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

NONAKA Satoshi¹,MUTO Tomotaro²,NAKAMURA Takahiro¹,NISHIDA Hiroyuki³

Affiliation:

1. Institute of Space and Astronautical Science, JAXA

2. Department of Aeronautics and Astronautics, The University of Tokyo

3. Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

General Medicine

Link

https://www.jstage.jst.go.jp/article/tastj/20/0/20_20.59/_pdf

Reference7 articles.

1. 1) Nonaka, S., Ogawa, H., and Inatani, Y.: Aerodynamic Design Considerations in Vertical Landing Rocket Vehicle, AIAA Paper 2001-1898, 2001.

2. 2) Nonaka, S., Imamura, Y., Shimotashiro, S., Ogawa, H., and Inatani, Y.: Turnover Maneuver of Vertical Landing Rocket Vehicle, 26th International Symposium on Space Technology and Science, Hamamatsu, Japan, 2008-g-20, 2008.

3. 3) Nonaka, S., Ito, T., Ogawa, H., and Inatani, Y.: Technologies and Verifications for Reusable Sounding Rocket System, 66th International Astronautical Congress, Jerusalem, Israel, IAC-15-D2.5.4, 2015.

4. 4) Ogawa, H., Nonaka, S., and Inatani, Y.: A Concept and Its Aerodynamic Design of a Sub-Orbital Reusable Rocket, 34th AIAA Fluid Dynamics Conference and Exhibit, AIAA 2004-2538, 2004.

5. 5) Suzuki, T., Nonaka, S., and Inatani, Y.: Computations of Opposing Jet from Vertical Landing Rocket Vehicle, AIAA Paper 2006-3329, 2006.