General & OtherAerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wAlan B Kehlet![Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta w]()
Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta w
Alan B Kehlet
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“Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta w” by Alan B…
Catalogue details
- Author
- Alan B Kehlet
- Category
- General & Other
- Language
- English
- Source
- HathiTrust