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Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination With a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2
Report discussing an investigation of the effect of sweepback angle on wing-fuselage characteristics at a subsonic and a supersonic Mach number. Lift, drag, and pitching-moment coefficients, downwash-angle, and total-pressure measurements are all provided.
Date:
June 6, 1951
Creator:
Luoma, Arvo A.
System:
The UNT Digital Library
The Crystal Structure of Uranium Tetrafluoride
Fourier refinement analysis of the uranium parameters in uranium tetrafluoride.
Date:
June 6, 1951
Creator:
Burbank, R. D.
System:
The UNT Digital Library