The theoretical characteristics of triangular-tip control surfaces at supersonic speeds Mach lines behind trailing edges
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Kainer, Julian H↗
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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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The Effect of Control Stiffness and Forward Speed on the Flutter of a 1/10-scale Dynamic Model of a Two-blade Jet-driven Helicopter Rotor
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Brooks, George W↗
Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics
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Williams, Walter C↗
Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degree Sweptback Wing and Tail as Obtained by the Transonic-bump Method
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Spearman, Leroy↗
A Wind-tunnel Investigation at Low Speed of Various Lateral Controls on a 45 Degree Swept-back Wing
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Hopkins, Edward J↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel V : Static Longitudinal Stability and Control Throughout the Subsonic Speed Range of a Semispan Model of a Supersonic Airplane
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Johnson, Ben H , Jr↗
Wind-tunnel Investigation of the Low-speed Longitudinal and Lateral Control Characteristics of a Triangular-wing Model of Aspect Ratio 2.31 Having Constant-chord Control Surfaces
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Wolhart, Walter D↗
Control Characteristics at Transonic Speeds of a Linked Flap and Spoiler on a Tapered 45 Degrees Sweptback Wing of Aspect Ratio 3
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Lockwood, Vernard E↗
Lateral-control investigation at transonic speeds of retractable spoiler and plug-type spoiler-slot ailerons on a tapered 60 degree sweptback wing of aspect ratio 2 : transonic-bump method
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Hammond, Alexander D↗
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↗
Low-speed Static Stability and Control Characteristics of a 1/4-scale Model of the Bell X-1 Airplane Equipped with a 4-percent-thick, Aspect-ratio-4, Unswept Wing
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Moseley, William C , Jr↗
A wind-tunnel investigation at high subsonic speeds of the lateral control characteristics of various plain spoiler configurations on a 3-percent-thick 60 degree delta wing
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of attack of -2 degrees to about 24 degrees to determine the lateral control characteristics of spoilers with various wing chord-wise and spanwise locations and spoiler spans and deflections on thin 60 degree delta wing of NACA 65a003 airfoil section parallel to free stream.
Wiley, Harleth G↗
Exploratory investigation of the moments on oscillating control surfaces at transonic speeds
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Martin, Dennis J↗
Simplified procedures for estimating flap-control loads at supersonic speeds
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Czarnecki, K R↗
Lateral-control Investigation at Transonic Speeds of Differentially Deflected Horizontal-tail Surfaces for a Configuration Having a 6-percent-thick 45 Degree Sweptback Wing
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Critzos, Chris C↗
Wind-tunnel investigation at transonic speeds of a jet control on a 35 degree swept wing : transonic-bump method
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Vogler, Raymond, D↗
Wind-tunnel investigation at transonic speeds of a jet control on an 80 degree delta-wing missile
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Turner, Thomas R↗
The use of cones as stabilizing and control surfaces at hypersonic speeds
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Love, Eugene S↗