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Results for “WINGS - SWEEPBACK”

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 415 records · Page 23

All sources NASA NTRS DOE OSTI

NASA NTRS1951

The Effects of Boundary-layer Control on the Longitudinal Characteristics of a Swept-back Wing Using Suction Through Streamwise Slots in the Outboard Portion of the Wing

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Mccormack, Gerald M↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-percent-thick, Biconvex Section

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Reese, David E↗

NASA NTRS1951

Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effectiveness at Supersonic Speeds of a 30-percent Chord, 50-percent Semispan Elevon as a Lateral Control Device

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Olson, Robert N↗

NASA NTRS1951

Flight Measurements of the Wing-dropping Tendency of a Straight-wing Jet Airplane at High Subsonic Mach Numbers

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Ernst, Edward A↗

NASA NTRS1951

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution

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Phelps, E Ray↗

NASA NTRS1951

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↗

NASA NTRS1951

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.8 to 1.6 of a Wing-body Combination Having an Unswept 4.5 Percent Thick Wing with Modified Hexagonal Sections

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Schult, Eugene D↗

NASA NTRS1951

A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

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Danforth, Edward C B↗

NASA NTRS1951

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Triangular Wing of Aspect Ratio 4 with 3-percent-thick, Biconvex Section

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Heitmeyer, John C↗

NASA NTRS1951

Contributions of Wing, Tail, and Fuselage to the Aerodynamic Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method

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Silsby, Norman S↗

NASA NTRS1951

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↗

NASA NTRS1951

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 3 with NACA 0003-63 section

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Heitmeyer, John C↗

NASA NTRS1951

The Effect on Zero-lift Drag of an Indented Fuselage or a Thickened Wing-root Modification to a 45 Degrees Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds

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Pepper, William B↗

NASA NTRS1951

Investigation of Minimum Drag and Maximum Lift-drag Ratios of Several Wing-body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds

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Brown, Clinton E↗

NASA NTRS1951

Pressure-distribution Measurements over a 45 Degree Sweptback Wing at Transonic Speeds by the NACA Wing-flow Method

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Danforth, Edward C B↗

NASA NTRS1951

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 4 with 3-percent-thick rounded nose section

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Heitmeyer, John C↗

NASA NTRS1952

The effectiveness of wing vortex generators in improving the maneuvering characteristics of a swept-wing airplane at transonic speeds

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Mcfadden, Norman M↗

NASA NTRS1951

The Use of Two-dimensional Section Data to Estimate the Low-speed Wing Lift Coefficient at which Section Stall First Appears on a Swept Wing

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Maki, Ralph L↗