59 research outputs found
Influence of Wing and Fuselage on the Vertical-tail Contribution to the Low-speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
Get PDFWind-tunnel Investigation at Low Speed of the Effects of Symmetrical Deflection of Half-delta Tip Controls on the Damping in Roll and Yawing Moment Due to Rolling of a Triangular-wing Model
Get PDFStatic Longitudinal Stability Characteristics of a Composite-plan-form Wing Model Including Some Comparisons with a 45 Degree Sweptback Wing at Transonic Speeds
Get PDFEffect of Sweepback on the Low-speed Static and Rolling Stability Derivatives of Thin Tapered Wings of Aspect Ratio 4
Get PDFStatic longitudinal and lateral stability characteristics at low speed of 60 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6
Get PDFExperimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degree Sweptback Wing and Tail Surfaces
Get PDFAn investigation was made to determine the effects of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with wing and vertical tails having the quarter-chord lines swept back 45 degrees. The results indicate that the directional instability of the various isolated fuselages was about two-thirds as large as that predicted by classical theory
Static Longitudinal and Lateral Stability Characteristics at Low Speed of Unswept-midwing Models Having Wings with an Aspect Ratio of 2, 4, or 6
Get PDFExperimental Investigation of the Low-speed Static and Yawing Stability Characteristics of a 45 Degrees Sweptback High-wing Configuration with Various Twin Vertical Wing Fins
Get PDFWind-tunnel investigation of the effects of horizontal-tail position on the low-speed longitudinal stability characteristics of an airplane model with a 35 degrees sweptback wing equipped with chordwise fences
Get PDFAn experimental investigation was made in the Langley stability tunnel to determine whether the low-speed longitudinal stability characteristics of a model with a 35 degree sweptback wing could be improved appreciably by lowering the horizontal tail. The investigation included tests of several components of the model and of various model configurations with chordwise fences on the wing
Some Effects of Amplitude and Frequency on the Aerodynamic Damping of a Model Oscillating Continuously in Yaw
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