Preliminary Results Of The Flight Investigation Between Mach Numbers Of 080 And 136 Of A Rocket Powered Model Of A Supersonic Airplane Configuration Having A Tapered Wing With Circular Arc Sections And 40c Sweepback
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Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback
| Author | : Charles T. D'Aiutolo |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1950 |
| Genre | : Stability of airplanes, Longitudinal |
| ISBN | : |
Download Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback Book in PDF, Epub and Kindle
