返回Google圖書搜尋

Distributed Educated Throat Stability Bypass to Increase the Stable Airflow Range of a Mach 2.5 Inlet with 60-percent Internal Contraction

Robert Joseph ShawGlenn A. MitchellBobby W. Sanders

出版	National Aeronautics and Space Administration, 1974
URL	http://books.google.com.hk/books?id=rsA4RX32rvwC&hl=&source=gbs_api

註釋The results of an experimental investigation to increase the stable airflow operating range of a supersonic mixed-compression inlet are presented. A distributed educated throat stability-bypass entrance configuration was tested. In terms of diffuser-exit corrected airflow, a large inlet stable airflow range of about 16.1 percent was obtained if a constant pressure was maintained in the bypass plenum. Limited unstart angle of attack data are presented.