타이틀 |
A Pressur Test of RCS Jet Interference at a Mach Numbere of 5 for a Tip Fin Configuration TM-714 |
저자 |
Shinji NAGAI, Koichi HOZUMI, Akira YOSHIZAWA, Nobutoshi HARA, Kiyomichi ISHIDA, Keisuke FUJII |
Keyword |
hypersonic flow; reaction control system; jet interference; tip fin |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm0000714.pdf?id=NALTM0000714 |
보고서번호 |
NAL TM-714 |
발행년도 |
1977.7 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
Aerodynamic interference induced by a reaction control system (RCS) jet was investigated for a tip fin configuration at a Mach number of 5. Surface pressure distributions and oil-flow photographs were obtained using cold gas simulation techniques with yaw jet scaled nozzles in the NAL φ50 cm hypersonic wind tunnel. It was found that the interference flow field changed as angles of atta |