Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the mach number range from 0.40 to 2.54/
| Main Author: | |
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| Corporate Authors: | , , |
| Format: | Book |
| Language: | English |
| Published: |
Washington, D.C.:
National Aeronautics and Space Administration ,
1976
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| Series: | NASA technical note
NASA TN D-8242 |
| Subjects: |
| Βιβλιοθήκη | Ταξιθετικός αριθμός | Αριθμός Αντιτύπων | Πληροφορίες | Κατάσταση |
|---|---|---|---|---|
| Δημοκρίτειο Πανεπιστήμιο Θράκης | TL 521 .3 | 1 | Προβολή | OPAC |