An Investigation At Mach Numbers From 020 To 463 Of The Aerodynamic Performance Static Stability And Trimming Characteristics Of A Canard Configuration Designed For Efficient Supersonic Cruise Flight
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An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight
Author | : |
Publisher | : |
Total Pages | : 88 |
Release | : 1961 |
Genre | : |
ISBN | : |
Download An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight Book in PDF, Epub and Kindle
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