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↗
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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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Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections
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Strass, H Kurt↗
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane 45 degree swept-back wing of aspect ratio 3, taper ratio 0.4 with 3-percent-thick, biconvex section
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Heitmeyer, John C↗
Comparison of Airfoil Sections on Two Triangular-wing-fuselage Configurations at Transonic Speeds from Tests by the NACA Wing-flow Method
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Hall, Albert W↗
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↗
Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an inboard elevon as a longitudinal- and lateral-control device at subsonic and supersonic speeds
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Pfyl, Frank A↗
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↗
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↗
Wing Load Distribution on a Swept Wing Airplane in Flight at Mach Numbers up to 1.11, and Comparison with Theory
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Rolls, L Stewart↗
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↗
Full-scale Wind-tunnel Investigation of the Effects of Wing Modifications and Horizontal-tail Location on the Low-speed Static Longitudinal Characteristics of a 35 Degree Swept-wing Airplane
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Maki, Ralph L↗
Low-speed Investigation of the Effects of Wing Leading-edge Modifications and Several Outboard Fin Arrangements on the Static Stability Characteristics of a Large-scale Triangular Wing
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Mclemore, H Clyde↗
Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : twisted and cambered triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution
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Heitmeyer, John C↗
An investigation of the low-speed longitudinal stability characteristics of a swept-wing airplane model with two modifications to the wing-root plan form
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Kemp, William B , 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↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch
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Robinson, Ross B↗
Transonic Drag Characteristics and Pressure Distribution on the Body of a Wing-body Combination Consisting of a Body of Revolution of Fineness Ratio 12 and a Wing Having Sweepback of 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoi
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Kurbjun, Max C↗
Aerodynamic Loading Characteristics of a Wing-fuselage Combination Having a Wing of 45 Degrees Sweepback Measured in the Langley 8-foot Transonic Tunnel
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Loving, Donald L↗