Effect of Taper Ratio on the Low-speed Rolling Stability Derivatives of Swept and Unswept Wings of Aspect Ratio 2.61
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Brewer, Jack D↗
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Wind-tunnel Investigation at Low Speeds of the Pitching Derivatives of Untapered Swept Wings
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Fisher, Lewis R↗
Ditching Tests of a 1/18-scale Model of the Lockheed Constellation Airplane.
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Morris, Garland J↗
Model Ditching Investigation of the Douglas DC-4 and DC-6 Airplanes
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Fisher, Lloyd J↗
Model ditching investigations of three airplanes equipped with hydro-skis
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Fisher, Lloyd J↗
Ditching Tests with a 1/16-size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail
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Fisher, Lloyd J↗
Low-speed static longitudinal and lateral stability characteristics of two low-aspect-ratio wings cambered and twisted to provide a uniform load at a supersonic flight condition
A delta wing and a tapered sweptback wing of aspect ratios 1.56 and 2.00, respectively, both of which were cambered and twisted so as to provide a uniform load distribution for a supersonic flight condition, were tested in combination with a fuselage at Reynolds numbers between 384,000 and 1,550,000 in order to determine the low-speed lift-drag and static stability characteristics of such wings.
REYNOLDS NUMBER EFFECTS - COMPLETE WINGS↗
An investigation of the effect of vertical-fin location and area on low-speed lateral stability derivatives of a semitailless airplane model
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Fisher, Lewis R↗
A Brief Hydrodynamic Investigation of a Navy Seaplane Design Equipped with a Hydro-ski
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Fisher, Lloyd J↗
Model Ditching Investigations of Three Airplanes Equipped with Hydro-skis
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Fisher, Lloyd J↗
Model Investigation of the Effect of Mounting Hydro-skis on Shock Absorbers
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Hoffman, Edward L↗
Experimental Determination of the Aerodynamic Derivatives Arising from Acceleration in Sideslip for a Triangular, a Swept, and an Unswept Wing
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Riley, Donald R↗
Experimental determination of the effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw
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Fisher, Lewis R↗
Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
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Aiken, William S , Jr↗
Horizontal-tail Parameters as Determined from Flight-test Tail Loads on a Flexible Swept-wing Jet Bomber
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Aiken, William S , Jr↗
Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model
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Fisher, Lewis R↗
Fabric fastenings
The study of aeronautical fabrics has led to a consideration of the best methods of attaching and fastening together such materials. This report presents the results of an investigation upon the proper methods of attaching fabrics to airplane wings. The methods recommended in this report have been adopted by the military services.
Walen, E D↗
Some Effects of Frequency on the Contribution of a Vertical Tail to the Free Aerodynamic Damping of a Model Oscillating in Yaw
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured tail-off and tail-on and compared with the values obtained by theoretical consideration of the unsteady lift associated with an oscillating vertical tail. A range of low frequencies comparable to those of the lateral motions of airplanes was covered. The analysis includes the effects of vertical-tail aspect ratio and the two-dimensional effects of compressibility.
Bird, John D↗