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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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At least 73 records · Page 4

All sources NASA NTRS DOE OSTI

NASA NTRS1954

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↗

NASA NTRS1952

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↗

NASA NTRS1954

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↗

NASA NTRS1954

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↗

NASA NTRS1956

Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds

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Yates, E Carson, Jr↗

NASA NTRS1957

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↗

NASA NTRS1958

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↗

NASA NTRS1948

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1949

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↗

NASA NTRS1950

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↗

NASA NTRS1950

Low-speed investigation of leading-edge and trailing-edge flaps on a 47.5 degree sweptback wing of aspect ratio 3.4 at a Reynolds number of 4.4 x 10(exp 6)

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Pasamanick, Jerome↗

NASA NTRS1950

Low-speed longitudinal characteristics of a circular-arc 52 degree sweptback wing of aspect ratio 2.84 with and without leading-edge and trailing-edge flaps at Reynolds numbers from 1.6 x 10(exp 6) to 9.7 x 10(exp 6)

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Foster, Gerald V↗

NASA NTRS1950

Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)

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Salmi, Reino J↗