An Investigation of a 0.16-scale Model of the Douglas X-3 Airplane to Determine Means of Improving the Low-speed Longitudinal Stability and Control Characteristics
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Mckee, John W↗
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Results for “LONGITUDINAL STABILITY”
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Preliminary flight measurements of the dynamic longitudinal stability characteristics of the Convair XF-92A delta-wing airplane
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Holleman, Euclid C↗
The Effects of Leading-edge Extensions, a Trailing-edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-fuselage-tail Combination Having a Wing with 35 Degrees of Sweepback and an Aspect Ratio of 4.5
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Selan, Ralph↗
Low-speed investigation of the effects of location of a delta horizontal tail on the longitudinal stability and control of a fuselage and thin delta wing with double slotted flaps including the effects of a ground board
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Riebe, John M↗
Free-flight Longitudinal-stability Investigation Including Some Effects of Wing Elasticity from Mach Numbers of 0.85 to 1.34 of a Tailless Missile Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 5.5
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Arbic, Richard G↗
A Transonic Wind-tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 0.09-scale Model of the Bell X-5 Research Airplane and Comparison with Flight
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Bielat, Ralph P↗
Relationship of flow over a 45 degree sweptback wing with and without leading-edge chord-extensions to longitudinal stability characteristics at Mach numbers from 0.60 to 1.03
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West, F E , Jr↗
A rocket-model investigation of the longitudinal stability, lift, and drag characteristics of the Douglas X-3 configuration with horizontal tail aspect ratio 4.33
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Peck, Robert F↗
The Effects of Fences on the High-speed Longitudinal Stability of a Swept-wing Airplane
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Bray, Richard S↗
Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6.0
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Mcfall, John C , Jr↗
A Flight Investigation at Mach Numbers from 0.67 to 1.81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Configuration Having an All-movable Tail
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Moul, Martin T↗
Effect of Reduction in Thickness from 6 to 2 Percent and Removal of the Pointed Tips on the Subsonic Static Longitudinal Stability Characteristics of a 60 Degree Triangular Wing in Combination with a Fuselage
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Palmer, William E↗
Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 x 10(exp 6).
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Foster, Gerald V↗
Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 degree delta-wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70
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Bond, Aleck C↗
The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations
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Mitchell, Jesse L↗
Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45 degrees sweptback wing and tail surfaces
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Lichtenstein, Jacob H↗
Effect of sweepback and aspect ratio on longitudinal stability characteristics of wings at low speeds
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Shortal, Joseph A↗
Static longitudinal stability and control characteristics of a 1/16 -scale model of the Douglas D-558-II research airplane at Mach numbers of 1.61 and 2.01
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Spearman, M Leroy↗