Compressive buckling of flat rectangular metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges
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Seide, Paul↗
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Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips subsonic leading edges and supersonic trailing edg
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Hannah, Margery E↗
Lift and Pitching Moment at Low Speeds of the Naca 64A010 Airfoil Section Equipped with Various Combinations of a Leading-edge Slat, Leading-edge Flap, Split Flap, and Double-slotted Flap
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Hayter, Nora-Lee F↗
Theoretical Supersonic Force and Moment Coefficients on a Sideslipping Vertical- and Horizontal-tail Combination with Subsonic Leading Edges and Supersonic Trailing Edges
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Malvestuto, Frank S , Jr↗
The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges
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Seide, Paul↗
Influence of Airfoil Trailing-edge Angle and Trailing-edge-thickness Variation on the Effectiveness of a Plain Flap at High Subsonic Mach Numbers
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Hemenover, Albert D↗
Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section
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Kelly, John A↗
Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds
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Yates, E Carson, Jr↗
Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing of aspect ratio 4
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Spreemann, Kenneth P↗
Low-speed Experimental Determination of the Effects of Leading-edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60 Degrees of Leading-edge Sweep
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Fletcher, Herman S↗
Free-flight Investigation of the Rolling Effectiveness at High Subsonic, Transonic, and Supersonic Speeds of Leading-edge and Trailing-edge Ailerons in Conjunction with Tapered and Untapered Plan Forms
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Strass, H Kurt↗
Hinge-moment measurements of a wing with leading-edge and trailing-edge flaps at a Mach number of 1.93
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Rainey, Robert W↗
Pressure-distribution Measurements over an Extensible Leading-edge Flap on Two Wings Having Leading-edge Sweep of 42 Degrees and 52 Degrees
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Salmi, Reino J↗
Full-scale Investigation of a Wing with the Leading Edge Swept Back 47.5 Degrees and Having Circular-arc and Finite-trailing-edge-thickness Ailerons
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Lange, Roy H↗
Effects of Systematic Changes of Trailing-edge Angle and Leading-edge Radius on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-percent-chord-thick NACA Airfoil Section
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Summers, James L↗
Two-dimensional Wind-tunnel Investigation of a 6-percent-thick Symmetrical Circular-arc Airfoil Section with Leading-edge and Trailing-edge High-lift Devices Deflected in Combination
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Nuber, Robert J↗
The Effect of Span and Deflection of Split Flaps and Leading-edge Roughness on the Longitudinal Stability and Gliding Characteristics of a 42 Degree Sweptback Wing Equipped with Leading-edge Flaps
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Pratt, George L↗
Full-scale Investigation of Boundary-layer Control by Suction Through Leading-edge Slots on a Wing-fuselage Configuration Having 47.5 Degree Leading-edge Sweep with and Without Flaps
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Pasamanick, Jerome↗