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RECOVERY OF URANIUM FROM GRAPHITE SHAPES BY ELECTROLYTIC GRAPHITE DISINTEGRATION IN NITRIC ACID
None
Date:
February 24, 1949
Creator:
Fromm, L.W.
System:
The UNT Digital Library
Experimental pressure distribution on a asymmetrical nonconical body at Mach number 1.90
Report presenting an investigation of the pressure distribution on an asymmetrical nonconical body at a Mach number of 1.90 over a wide range of angles of attack and yaw. Pressure distributions occurred at anticipated trends. Results regarding the pressure coefficients, Schileren photographs, boundary layers, and pressure distributions are provided.
Date:
February 24, 1949
Creator:
Wyatt, DeMarquis D.
System:
The UNT Digital Library
Aerodynamic Characteristics of a Wing With Quarter-Chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section: Transonic-Bump Method
Report discussing a particular wing-body combination that is part of a larger investigation to determine the lift, drag, pitching moment, and root bending moments for various configurations. Information about the aerodynamic characteristics at the tail plane is also provided.
Date:
February 24, 1949
Creator:
Weil, Joseph & Goodson, Kenneth W.
System:
The UNT Digital Library