Effect of skewed wing-tip controls on a variable-sweep wing-fuselage configuration
Skewed wing tip control effects on variable sweep wing-fuselage configuration
WING TIP CONTROL↗
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Results for “WINGS - AEROELASTICITY”
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Effect of wing pivot location on longitudinal aerodynamic characteristics of a variable sweep wing having an M planform
Wing pivot location effect on longitudinal aerodynamic characteristics of variable sweep wing having M planform
VARIABLE SWEEP↗
Investigation of Wing Characteristics at a Mach Number of 1.53 II : Swept Wings of Taper Ratio 0.5
Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings varying in sweep angle from 60 degrees sweepforward to 60 degrees sweepback. All wings had a cambered, double-wedge section 5-percent thick and a common taper ratio of 0.5. The experimental results are compared with the predictions of the linear theory.
WINGS, COMPLETE - THEORY↗
FREE-FLIGHT TESTS OF 45 DEG SWEPT WINGS OF ASPECT RATIO 3.15 AND TAPER RATIO 0.54 TO MEASURE WING DAMPING OF THE FIRST BENDING MODE AND TO INVESTIGATE THE POSSIBILITY OF FLUTTER AT TRANSONIC SPEEDS
Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter
FLUTTER↗
Low-Speed Investigation Of The Effects Of Horizontal-Tail Area And Wing Sweep On The Static Longitudinal Stability And Control Characteristics Of An Airplane Configuration Having Tail Surfaces Outboard Of The Wing Tips
Low-speed longitudinal static stability & control characteristics of aircraft with swept wings & tail surfaces outboard of wing tips
STABILITY AND CONTROL↗
Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75 deg
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 degrees at Mach 2.01
SWEPT WING↗
Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 deg delta wing
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01
DELTA WING↗
Effect of wing planform modification on longitudinal characteristics of a variable- sweep m wing
Wind tunnel testing to determine effects of wing planform modifications on longitudinal aerodynamic characteristics of variable-sweep M planform wing
WIND TUNNEL STABILITY TEST↗
Effect of wing leading-edge shape on aerodynamic characteristics of a 67 deg swept wing-body model at Mach 1.50 to 4.63
Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63
SUPERSONIC SPEED↗
An integrated approach to the analysis and design of wings and wing-body combinations in supersonic flow
Numerical procedure for analyzing and designing wings and wing-body combinations in supersonic flow
SUPERSONIC FLOW↗
Wing-body Combinations with Wings of Very Low Aspect Ratio at Supersonic Speeds
Wing-body combinations with wings of very low aspect ratio at supersonic speeds
TAIL↗
Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 deg swept arrow wing model with variations in horizontal-tail height, wing height, and dihedral
Horizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model
DIHEDRAL EFFECT↗
The Effect of Negative Dihedral, Tip Droop, and Wing-tip Shape on the Low-speed Aerodynamic Characteristics of a Complete Model Having a 45 Degrees Sweptback Wing
An investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing. Longitudinal and lateral stability characteristics were obtained for the model with and without tail surfaces.
STABILITY, LONGITUDINAL - STATIC↗
Calculation of combining effects in the structure of airplane wings: a rational basis for estimating the reduction in the design load on wing beams due to the influence of ribs and covering toward causing the beams to deflect together
This lecture concerns the combining effects in airplane wings so as to save some of the dead weight.
WING RIBS↗
A TABULATION OF WIND-TUNNEL PRESSURE DATA AND SECTION AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS OF 1.61 AND 2.01 FOR A REFLEX CAMBERED WING AND A CAMBERED AND TWISTED WING HAVING THE SAME SWEPT PLANFORM
Tabulation of wind tunnel pressure data and section aerodynamic characteristics for a reflex cambered wing
TWISTED WING↗
Aerodynamic characteristics in pitch of a modified half ring wing body combination and a swept wing body combination at Mach 2.16 to 3.70
Wind tunnel stability tests of pinch of modified half ring wing body and swept wing body combinations at supersonic speeds
Lamb, M.↗
Effects of simulated wing damage on the aerodynamic characteristics of a swept-wing airplane model
Simulated wing damage effects on aerodynamic characteristics of swept-wing airplane model
Hayes, C.↗
Exploratory investigation of the structure of the tip vortex of a semispan wing for several wing-tip modifications
Wind tunnel investigation of tip vortex structure of semispan wing for several wing-tip modifications
Scheiman, J.↗