Effect of a Deflectable Wing-tip Control on the Low-speed Lateral and Longitudinal Characteristics of a Large-scale Wing with the Leading Edge Swept Back 47.5 Degrees
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Lange, Roy 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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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↗
Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Chordwise Positions at the Wing Tip of a 45 Degrees Sweptback Wing and Body Combination
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Pepper, William B , Jr↗
Wind-tunnel Investigation at Low Speed of the Effects of Symmetrical Deflection of Half-delta Tip Controls on the Damping in Roll and Yawing Moment Due to Rolling of a Triangular-wing Model
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Wolhart, Water D↗
Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
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Hoffman, Sherwood↗
Low-speed Wind-tunnel Investigation of Lateral Control Characteristics of a 60 Degrees Triangular-wing Model Having Half-delta Tip Controls
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Jaquet, Byron M↗
Derivation of the equations of motion of a symmetrical wing-tip-coupled airplane configuration with rotational freedom at the junctures
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Source record↗
Flight Investigation at Subsonic, Transonic, and Supersonic Velocities of the Hinge-moment Characteristics, Lateral-control Effectiveness, and Wing Damping in Roll of a 60 Degrees Sweptback Delta Wing with Half-delta Tip Ailerons
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Martz, C William↗
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed I : turbine-design requirements for several engine operating conditions
In order to insure satisfactory turbine performance under five turbojet-engine operating conditions, turbine design requirements were determined for the following operating conditions: take-off, maximum thrust at altitude, altitude cruising at rated rotative speed, altitude cruising with maximum-thrust exhaust nozzle area, and engine acceleration at 80 percent equivalent design rotative speed. If cruising is to be at rated engine speed, both cruising and take-off should be considered in turbine design. Design requirements for the other conditions are nearly identical. Without compressor-exit bleed, a turbine cannot accelerate this compressor at 80 percent of rated speed; with 28.6-percent bleed, the design requirements are within those for take-off.
TURBINES--AXIAL FLOW↗
Low-speed Wind-tunnel Investigation of a Fixed and a Free-floating Wing-tip Aileron on a Wing with Leading Edge Swept Back 51.3 Degrees
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Macleod, R G↗
Free-flight Investigation to Determine Force and Hinge-moment Characteristics at Zero Angle of Attack of a 60 Degrees Sweptback Half-delta Tip Control on a 60 Degrees Sweptback Delta Wing at Mach Numbers Between 0.68 and 1.44
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Martz, C William↗
Investigation of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by the transonic-bump method
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Moseley, William C , Jr↗
The calculation of certain static aeroelastic phenomena of wings with tip tanks or boom-mounted lifting surfaces
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Diederich, Franklin W↗
Aerodynamic Characteristics at Transonic Speeds of a Wing Having a 45 Degree Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip.
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Morrison, William D , Jr↗
The Effect of Raking the Aileron Tips on the Lateral-control and Hinge-moment Characteristics of a 20-percent-chord Partial-span Outboard Aileron on a Wing with Leading-edge Swept Back 51.3 Degrees
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Hammond, Alexander D↗
Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degree Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips
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Hoffman, Sherwood↗
An Investigation of Longitudinal Control Characteristics of a Wing-tip Control Surface on a Sweptback Wing at Transonic Speeds by the NACA Wing-flow Method
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Trant, James P , Jr↗
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↗