Low-speed static lateral stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
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Bates, William R↗
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Theoretical Investigation of the Dynamic Lateral Stability Characteristics of the Douglas X-3 Research Airplane : Study 41-B
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Bennett, Charles V↗
Low-speed Lateral Stability and Aileron-effectiveness Characteristics at a Reynolds Number of 3.5 x 10(exp 6) of a Wing with Leading-edge Sweepback Decreasing from 45 Degrees at the Root to 20 Degrees at the Tip
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Lange, Roy H↗
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Static Lateral Stability Characteristics at Mach Numbers of 1.40 and 1.59
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Spearman, M Leroy↗
Calculations of the dynamic lateral stability characteristics of the Douglas D-558-II airplane in high speed flight for various wing loadings and altitudes
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Queijo, M J↗
The effect of mass distribution on the low-speed dynamic lateral stability and control characteristics of a model with a 60 degree triangular wing
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Johnson, Joseph L↗
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↗
Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a tip-to-tip bomber-fighter coupled airplane configuration
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Bennett, Charles V↗
Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with self-supporting free-floating fuel tanks attached to the wing tips
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Bennett, Charles V↗
Static lateral stability characteristics of a 1/10-scale model of the X-1 airplane at high subsonic Mach numbers
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Kuhn, Richard E↗
Flight measurements of the lateral stability and control characteristics of a high-speed fighter airplane
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Crane, H L↗
Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with a sweptback-wing fighter model attached to each wing tip
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Bennett, Charles V↗
Wind-tunnel Investigation of the Static Lateral Stability Characteristics of Wing-fuselage Combinations at High Subsonic Speeds : Sweep Series
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Kuhn, Richard E↗
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Model with Leading-edge Chord-extensions Incorporated on a 40 Degree Sweptback Circular-arc Wing of Aspect Ratio 4 and Taper Ratio 0.50
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Goodson, Kenneth W↗
An analysis of the lateral stability of the Douglas D-558-II airplane equipped with a yaw damper, with special reference to the effect of yaw-damper rate-gyro spin-axis orientation
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Gates, Ordway B , Jr↗
Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high subsonic speeds : aspect-ratio series
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Fournier, Paul G↗
Static Lateral Stability Characteristics of an Airplane Model Having a 47.7 Degree Sweptback Wing of Aspect Ratio 6 and the Contribution of Various Model Components at a Reynolds Number of 4.45 x 10(exp 6)
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Griner, Roland F↗