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[American Institute of Aeronautics and Astronautics 9th Propulsion Conference - Las Vegas,NV,U.S.A. (05 November 1973 - 07 November 1973)] 9th Propulsion Conference - Design of maximum thrust nozzles for nonequilibrium, chemically reacting flow

✍ Scribed by TAYLOR, A.; HOFFMAN, J.

No coin nor oath required. For personal study only.

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