타이틀 |
Wind tunnel Investigation of an STOL Aircraft Model (An effefct of engine nacelle shape) |
저자 |
wind Tunnel Investigation of an STOL Aircraft Model (An effefct of engine nacelle shape |
Keyword |
Engine nacelle; STOL aircraft model; Wind tunnel test |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00653.pdf?id=NALTM0000653 |
보고서번호 |
NAL TM-653 |
발행년도 |
1993.1 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
In initial wind tunnel tests on STOL experimental aircraft developed and researched by the National Aerospace Laboratory, a simulator engine nacelle which is longer and larger than that of 8% scales of FJR engines used in actual aircraft, was installed and tested on a model. To estimate ASKA′s aerodynamics force data from wind tunnel data, the data |