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Results for “AILERONS - DISPLACEMENT”

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 325 records · Page 18

All sources NASA NTRS DOE OSTI

NASA NTRS1950

Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds

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Thompson, Robert F↗

NASA NTRS1951

Wind-tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle with Three Untapered 45 Degree Sweptback Wings

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Johnson, Harold S↗

NASA NTRS1950

Low-speed Investigation of the Effect of Several Flap and Spoiler Ailerons on the Lateral Characteristics of a 47.5 Degree Sweptback-wing-fuselage Combination at a Reynolds Number of 4.4. x 10(6)

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Pasamanick, Jerome↗

NASA NTRS1951

Experimental Study of the Effect of Sweepback on Transonic Aileron Flutter

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Levy, Lionel L , Jr↗

NASA NTRS1951

Free-flight Measurements at Mach Numbers from 0.7 to 1.6 of Some Effects of Airfoil-thickness Distribution and Trailing-edge Angle on Aileron Rolling Effectiveness and Drag for Wings with 0 and 45 Degrees Sweepback

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Fields, E M↗

NASA NTRS1951

Investigation of low-speed lateral control and hinge-moment characteristics of a 20-percent-chord plain aileron on a 47.7 degrees sweptback wing of aspect ratio 5.1 at a Reynolds number of 6.0 x 10(exp 6)

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Hadaway, William M↗

NASA NTRS1951

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↗

NASA NTRS1951

Comparison of Semispan and Full-span Tests of a 47.5 Degrees Sweptback Wing with Symmetrical Circular-arc Sections and Having Drooped-nose Flaps, Trailing-edge Flaps, and Ailerons

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Lipson, Stanley↗

NASA NTRS1952

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↗

NASA NTRS1951

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↗

NASA NTRS1952

Low-speed Aerodynamic Characteristics of a Large-scale 45 Degree Swept-back Wing with Partial-span Slats, Double-slotted Flaps, and Ailerons

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James, Harry A↗

NASA NTRS1952

Lateral-control investigation at transonic speeds of retractable spoiler and plug-type spoiler-slot ailerons on a tapered 60 degree sweptback wing of aspect ratio 2 : transonic-bump method

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Hammond, Alexander D↗

NASA NTRS1952

The Effect of Various Aerodynamic Balances on the Low-speed Lateral-control and Hinge-moment Characteristics of a 0.20-chord Partial-span Outboard Aileron on a Wing with Leading Edge Swept Back 51.3 Degrees

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Hammond, Alexander D↗

NASA NTRS1952

Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons

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Hammond, Alexander, D↗

NASA NTRS1952

Low-speed lateral-control investigation of a flap-type spoiler aileron with and without a deflector and slot on a 6-percent-thick, tapered, 45 degree sweptback wing of aspect ratio 4

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Watson, James M↗

NASA NTRS1953

A Free-flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments

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Bland, William M , Jr↗

NASA NTRS1953

Free-spinning-tunnel investigation of a model having a 60 degrees delta wing with half-delta ailerons installed

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Klinar, Walter J↗

NASA NTRS1953

Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight

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Drake, Hubert M↗