Analysis of sweptback wings on Cal-Tech analog computer
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Macneal, Richard H↗
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Results for “WINGS, SWEPTBACK - CHARACTERISTICS”
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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Theoretical investigation of the supersonic lift and drag of thin, sweptback wings with increased sweep near the root
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Cohen, Doris↗
Low-speed Wind-tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing
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Keith, Arvid L , Jr↗
A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model
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Foster, Gerald V↗
Investigation at High Subsonic Speeds of a Body-contouring Method for Alleviating the Adverse Interference at the Root of a Sweptback Wing
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Mcdevitt, John B↗
Full-scale Wind-tunnel Tests of a 35 Degree Sweptback-wing Airplane with Blowing from the Shroud Ahead of the Trailing-edge Flaps
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Tolhurst, William H , Jr↗
Low-speed pressure distributions over the drooped-nose flap of a 42 degrees sweptback wing with circular-arc airfoil sections at a Reynolds number of 5.3 x 10(exp 6)
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Woods, Robert L↗
Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds
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Turner, Thomas R↗
Downwash, sidewash, and wake surveys behind a 42 degrees sweptback wing at a Reynolds number of 6.8 x 10(exp 6) with and without a simulated ground
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Furlong, Chester G↗
High-speed wind-tunnel investigation of a sweptback wing with an added triangular area at the center
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Henry, Beverly, Z , jr↗
Effect of Airfoil Profile of Symmetrical Sections on the Low-speed Static-stability and Yawing Derivatives of 45 Degrees Sweptback Wing Models of Aspect Ratio 2.61
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Letko, William↗
Effect of airfoil profile of symmetrical sections on the low-speed rolling derivatives of 45 degree sweptback-wing models of aspect ratio 2.61
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Letko, William↗
Lateral-control Investigation on a 37 Degree Sweptback Wing of Aspect Ratio 6 at a Reynolds Number of 6,800,000
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Koven, William↗
Preliminary Investigation of Spoiler Lateral Control on a 42 Degree Sweptback Wing at Transonic Speeds
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Schneiter, Leslie E↗
Flight Investigation to Determine the Hinge Moments of a Beveled-edge Aileron on a 45 Degree Sweptback Wing at Transonic and Low Supersonic Speeds
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Gardner, William N↗
Investigation of Pressure Distribution over an Extended Leading-Edge Flap on a 42 Degrees Sweptback Wing
Pressure distribution over an extended leading-edge flap on a 42 degree swept-back wing was investigated. Results indicate that the flap normal-force coefficient increased almost linearly with the angle of attack to a maximum value of 3.25. The maximum section normal-force coefficient was located about 30 percent of the flap span outboard of the inboard end and had a value of 3.75. Peak negative pressures built up at the flap leading edge as the angle of attack was increased and caused the chordwise location of the flap center of pressure to be move forward.
Conner, D. William↗
Experimental and calculated hinge moments of two ailerons on a 42.7 degrees sweptback wing at a Mach number of 1.9
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Goin, Kennith L↗
A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model
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Foster, Gerald V↗