Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet/
Main Author: | |
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Corporate Authors: | , , |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
NASA, Scientific and Technical Information Office,
1980
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Series: | NASA technical paper
1532 |
Subjects: |
Βιβλιοθήκη | Ταξιθετικός αριθμός | Αριθμός Αντιτύπων | Πληροφορίες | Κατάσταση |
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Δημοκρίτειο Πανεπιστήμιο Θράκης | TL 521 .3 | 1 | Προβολή | OPAC |