타이틀 |
Measurements of Engine Exhaust Flow in USB-STOL Semi-span Aircraft Model by CAD-Influence of Space between Engines on Turning Characteristics of Engine Exhaust Flow- |
저자 |
Hirotoshi FUJIEDA, Toshimi FUJITA, Akihito IWASAKI, Hitoshi TAKAHASHI, Masahiro OKUYAMA |
Keyword |
Wake measurement; USB aircraft model; Lows-peed wind tunnel test |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00682.pdf?id=NALTM0000682 |
보고서번호 |
NAL TM-682 |
발행년도 |
1995.4 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
The wake measurements were made to investigate the influence of the space between engines on the turning performance of two exhaust flows in an Upper Surface Blowing(USE)type powered Iift aircraft.The test model was a semi-span model equipped with two engines on the wing.The experiments were conducted for three spaces between engines by moving spa |