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A flight investigation of the effect of leading-edge camber on the aerodynamic characteristics of a swept-wing airplane
Report presenting flight measurements on a swept-wing jet aircraft to determine the effects of adding forward camber and an increased leading-edge radius on the low-speed stalling characteristics, the high-speed static longitudinal stability, and the airplane drag. The modified leading edge produced values of maximum lift somewhat greater than the slats on a normal airplane, but the stall was unacceptable because of an abrupt roll-off.
Date:
February 18, 1953
Creator:
Anderson, Seth B.; Matteson, Frederick H. & Van Dyke, Rudolph D., Jr.
System:
The UNT Digital Library
Effect of vertical position of the wing on the aerodynamic characteristics of three wing-body combinations
Report presenting the results of an experimental investigation of three plane wings in combination with a body, which represented both low- and high-wing arrangements. The three wings had different plan forms: a tapered unswept plan form, a tapered 45 degree sweptback plan form, and a triangular plan form. Results regarding the effect of Reynolds number and effect of vertical position of the wing are provided.
Date:
February 18, 1953
Creator:
Heitmeyer, John C.
System:
The UNT Digital Library
Some Basic Properties of Barium Titanate
None
Date:
February 18, 1953
Creator:
Stuart, T. P.
System:
The UNT Digital Library
Medical and Health Physics Quarterly Report: October, November, and December, 1952
Report of progress on the metabolic properties of various materials, biological studies of radiation effects, health chemistry and physics.
Date:
February 18, 1953
Creator:
University of California Radiation Laboratory
System:
The UNT Digital Library