Investigation of the Dynamic Longitudinal Stability of Two Equal Size Models Coupled in Tandem with a Single Joint;Preliminary Model Flight Tests
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Shanks, Robert E↗
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Dynamic longitudinal stability and control of tandem coupled bomber-fighter airplane models with rigid and pitch-free coupling
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Granda, David C↗
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↗
Static Longitudinal Stability and Dynamic Characteristics at High Angles of Attack and at Low Reynolds Numbers of a Model of the X-3 Supersonic Research Airplane
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Burk, Sanger M↗
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↗
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↗
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 static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations
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Mitchell, Jesse L↗
A Flight Investigation of the Effects of Inclination of the Principal Axis of Inertia on the Dynamic Lateral Stability of the Republic XF-91 Airplane
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Finch, Thomas W↗
Flight measurements of the dynamical longitudinal stability and frequency-response characteristics of the XF-92A delta-wing airplane
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Holleman, Euclid C↗
Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail
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Beam, Benjamin H↗
Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane
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Campbell, John P↗
The Static and Dynamic-rotary Stability Derivatives at Subsonic Speeds of an Airplane Model with an Unswept Wing and a High Horizontal Tail
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Buell, Donald A↗
Dynamic directional stability derivatives for a 45 degree swept-wing-vertical-tail airplane model at transonic speeds and angles of attack, with a description of the mechanism and instrumentation employed
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Albert L. Braslow↗
Dynamic Longitudinal Stability Characteristics of a Swept-wing Fighter-type Airplane at Mach Numbers Between 0.36 and 1.45
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Wolowicz, Chester H↗
The Static and Dynamic-rotary Stability Derivatives at Subsonic Speeds of a Model of the X-15 Research Airplane
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Lopez, Armando E↗
Static and Dynamic-rotary Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail at Mach Numbers of 2.5, 3.0, and 3.5
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Lampkin, Bedford A↗