Wind-tunnel Investigation of Effects of Ground Proximity and of Split Flaps on the Lateral Stability Derivatives of a 60 Degree Delta-wing Model Oscillating in Yaw
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Jaquet, Byron M↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A method utilizing data on the spiral, roll-subsidence, and dutch roll modes for determining lateral stability derivatives from flight measurements
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Klawans, Bernard B↗
Wind-tunnel Investigation of the Static Lateral Stability Characteristics of Wind-fuselage Combinations at High Subsonic Speeds : Taper-ratio Series
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Wiggins, James W↗
Static 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
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Wolhart, Walter D↗
Low-speed Experimental Determination of the Effects of Leading-edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60 Degrees of Leading-edge Sweep
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Fletcher, Herman S↗
The Effects of Fuel Sloshing on the Lateral Stability of a Free-flying Airplane Model
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Smith, Charles C , Jr↗
Experimental Determination of the Lateral Stability of a Glider Towed by a Single Towline and Correlation with an Approximate Theory
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Maggin, Bernard↗
Langley Free-flight-tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided Either Flicker-type or Hunting Control
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Schade, Robert O↗
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↗
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↗
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↗
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↗
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↗