Air Intake Development for Supersonic Missiles-Reference-Cited by-同舟云学术

Air Intake Development for Supersonic Missiles

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Kurth Guido,Bauer Christoph

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. 1Besser, H.L. "HistoryofDuctedRocket DevelopmentatBayern-Chemie", 44rd AIAA/ASME/SAE/ASEE JointPropulsion Conference, HartfordCT,July2008

2. 3Pohl, W.D. and Krohn, E.O. "Multiple-Inlet Configuration for Missiles with Skid-to-Turn Control Mode"; AGARD ConferenceProceedings,AGARD-CP-526,Paper24,May1992.

3. Efficient solution algorithms for the Riemann problem for real gases

4. The Piecewise Parabolic Method (PPM) for gas-dynamical simulations

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