Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
Renaldo V Jenkins
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“Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel” by Renaldo V…
Catalogue details
- Author
- Renaldo V Jenkins
- Category
- General & Other
- Language
- English
- Source
- HathiTrust