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Results for “AILERONS - DEFLECTION”

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 163 records · Page 9

All sources NASA NTRS DOE OSTI

NASA NTRS1950

Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow

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WINGS - AIR FORCES↗

NASA NTRS1928

Aerodynamic characteristics of thin empirical profiles and their application to the tail surfaces and ailerons of airplanes

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AIRFOILS, THIN - CHARACTERISTICS↗

NASA NTRS1944

A Theoretical Investigation of the Rolling Oscillations of an Airplane with Ailerons Free

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MOMENTS OF INERTIA↗

NASA NTRS1943

Flight measurements of the effect of various amounts of aileron droop on the low-speed lateral-control characteristics of an observation airplane

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SIDESLIPPING - VOUGHT-SIKORSKY OS2U-2↗

NASA NTRS1945

Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel I : Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements

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WINGS - CONSOLIDATED VULTEE B-36 WIND TUNNEL TESTS↗

NASA NTRS1944

Longitudinal Characteristics and Aileron Effectiveness of a Midwing Airplane from High-Speed Wind Tunnel Tests

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PRESSURE DISTRIBUTION- WINGS-DOUGLAS B-42↗

NASA NTRS1944

Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed

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ROLLING↗

NASA NTRS1945

A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

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AILERON CONTROLS↗

NASA NTRS1943

Limitations of lifting-line theory for estimation of aileron hinge-moment characteristics

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AILERONS - HINGE MOMENTS↗

NASA NTRS1949

The rolling power of two wing-aileron configu- rations as affected by flexibility

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Purser, P. E.↗

NASA NTRS1969

Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model

Wind tunnel studies of scaled model of multijet cargo airplane

Abel, I.↗

NASA NTRS1954

Free-flight investigation of the full-scale Hughes Falcon missile, D configuration, to determine aileron effectiveness and damping in roll

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Lundstrom, R. R.↗

NASA NTRS1924

The induction factor used for computing the rolling moment due to the ailerons

In the following note, prepared for the National Advisory Committee for Aeronautics, this induction factor is determined from the result of a model test, and compared with a formula recently developed by the author. The two results are found to be in substantial agreement.

Munk, Max M↗

NASA NTRS1946