Aerodynamic characteristics of a hypersonic research airplane concept having a 70o swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0/
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Corporate Authors: | , , |
Other Authors: | |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1979
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Series: | NASA technical paper
1552 |
Subjects: |
Βιβλιοθήκη | Ταξιθετικός αριθμός | Αριθμός Αντιτύπων | Πληροφορίες | Κατάσταση |
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Δημοκρίτειο Πανεπιστήμιο Θράκης | TL 521 .3 | 1 | Προβολή | OPAC |