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Measurement of Flying Qualities of a Douglas A-26B Airplane (AAF No. 41-39120) 1: Longitudinal Stability and Control Characteristics
Report discussing testing of the Douglas A-26B to determine the longitudinal stability and control characteristics. Information about the elevator, stick-fixed and stick-free stability, center of gravity, and flap effects are described.
Date:
December 6, 1944
Creator:
Crane, H. L.; Sjoberg, S. A. & Hoover, H. H.
System:
The UNT Digital Library
Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped With a Low-Drag Wing
Report discussing flight tests on a low-drag wing pursuit airplane to determine the effects of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls. The obtainable maximum lift coefficient was found to be greatly affected by the Mach and Reynolds numbers in gradual stall. In abrupt stalls, the maximum lift coefficient was affected by the Mach number, but not the Reynolds number.
Date:
July 6, 1945
Creator:
Spreiter, John R.; Galster, George M. & Blair, William K.
System:
The UNT Digital Library
Knock-Limited Performance of Blends of AN-F-28 Fuel Containing 2 Percent Aromatic Amines 5
Report discussing testing of 2-percent additions of seven aromatic amines on the knock-limited performance of 28-R fuel in a CFR engine. The most effective antiknock additives are described.
Date:
August 6, 1945
Creator:
Alquist, Henry & Tower, Leonard K.
System:
The UNT Digital Library