Title: Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane I : two-dimensional compression-ramp inlets with semicircular cowls
Publication Year: 1952
Publication Date: 1952-07-16
Language: en
Type: article
Access and Citation
AI Researcher Chatbot
Get quick answers to your questions about the article from our AI researcher chatbot