Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86/
| Main Author: | |
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| Corporate Authors: | , , |
| Format: | Book |
| Language: | English |
| Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1979
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| Series: | NASA technical paper
1539 |
| Subjects: |
| Βιβλιοθήκη | Ταξιθετικός αριθμός | Αριθμός Αντιτύπων | Πληροφορίες | Κατάσταση |
|---|---|---|---|---|
| Δημοκρίτειο Πανεπιστήμιο Θράκης | TL 521 .3 | 1 | Προβολή | OPAC |