Engineering & TechnologyAerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a boCarlton S James![Aerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a bo]()
Aerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a bo
Carlton S James
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“Aerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a bo” by Carlton S…
Catalogue details
- Author
- Carlton S James
- Category
- Engineering & Technology
- Language
- English
- Source
- HathiTrust