Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results
| Author | : |
| Publisher | : |
| Total Pages | : 120 |
| Release | : 1960 |
| ISBN-10 | : NASA:31769000459795 |
| ISBN-13 | : |
| Rating | : 4/5 ( Downloads) |
Book Synopsis Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results by :
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