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General & OtherAerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnelRenaldo V JenkinsAerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel

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

About this book

“Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel” is a book by Renaldo V Jenkins in the “General & Other” category, written in English. It is in the public domain, so you can read it for free from the open source using the buttons above. If you enjoyed it, press Like to help others find it. Similar books are listed below.

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