Cross Section Controllable Hypersonic Inlet Design Using Streamline-Tracing and Osculating Axisymmetric Concepts AIAA Paper
43rd, Joint propulsion conference ; 2007 ; Cincinnati, OH
2007-01-01
3373 pages
Papers in the range 2007 5004 to 5862. Held on CD-ROM
Aufsatz (Konferenz)
Englisch
Propulsion , AIAA , ASME , SAE , ASEE
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