Dynamic Response Of A Mach 2 5 Axisymmetric Inlet And Turbojet Engine With A Poppet Value Controlled Inlet Stability Bypass System When Subjected To Internal And External Airflow Transients
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Aeronautical Engineering
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).