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Synonyme wurden verwendet für: Motion • vibration • vibration control
Suche ohne Synonyme: title: Motion and vibration control

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    The Constantinesco Torque-Converter

    JACK, R. K. | SAE Technical Papers | 1927
    of the stick and also alters the amplitude and rate of vibration of all parts. At the same time, pressure is set up at the point of ...

    Some Books Recently Received

    Emerald Group Publishing | 1936
    . All branches of the subject which relate to the steady motion of the aeroplane are touched on. Stability and control and disturbed motion ...

    Flight Tests of an Airplane Showing Dependence of the Maximum Lift Coefficient on the Test Conditions

    Soule, H A / Hootman, James A | NTRS | 1937
    loading at which the tests were made, the position or motion of the propeller, and the rate at which the angle of attack is changing when the ...
    Verlag: NASA National Aeronautics and Space Administration

    Month in the Patent Office

    Emerald Group Publishing | 1939
    in the normal mean position of the blade intersects the axis of rotation at the mean centre of oscillation F of the blade pitch control gear ...

    Control-Surface Instability on High-Speed Airplanes

    Phillips, William H. | NTRS | 1942
    ailerons suddenly overbalanced. The efforts of the pilot to bring the ailerons back to neutral resulted in a violent oscillation of the control ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Stability And Control

    DYNAMICALLY STABLE SPRING SUSPENSION for Railway Cars and Motorcoaches

    LINDVALL, F. C. / BEEMER, PAUL K. | SAE Technical Papers | 1942
    normal service. Lateral movement of the body floating on the main springs is restrained by control arms and links which act on the body above the ...

    Aerodynamic Tests of a Full-scale TBF-1 Aileron Installation in the Langley 16-foot High-Speed Tunnel

    Becker, John V / Korycinski, Peter F | NTRS | 1944
    oscillation of the wing and flapping of the aileron. The aileron motion appeared to be coupled with the motion of the wing through the mass unbalance ...
    Verlag: NASA National Aeronautics and Space Administration

    Investigations on stability, oscillation, and stress conditions of airplanes with tab control. First partial report -- Derivation of equations of motion and their general solutions

    Filzek, B. | Engineering Index Backfile | 1949

    Investigations on the stability, oscillation, and stress conditions of airplanes with tab control. Second partial report : application of the solutions obtained in the first partial report to tab-controlled airplanes.

    Filzek, B | NTRS | 1949
    The first partial report, FB 2000, contained a discussion of the derivation of the equations of motion and their solutions for a tab ...
    Verlag: NASA National Aeronautics and Space Administration

    Flight Proofing Test Report of Ass'y-Rate Gyro, Autopilot (Two Axis Rate Gyro Group) DWG. No. 27-41770 Prototype Ser. No. 1

    D. D. Blanchard | NTIS | 1960
    . Testing was performed in accordance with the Flight Proofing Test Procedure and the results are contained herein. (Author) ...
    Schlagwörter: Vibration , Pitch(Motion) , Navigation, Guidance, & Control

    National Specialists Meeting on Guidance of Aerospace Vehicles -- Proc

    Engineering Index Backfile | 1960
    Papers presented at Boston, Mass, May 25-27 1960: Command and Data Link for Astronomical Satellite L.L.ANTES 5-13; Guidance and Control ...

    Instrumentation Configuration Summary (Flight Missiles) E Series

    NTIS | 1960
    control system, new pneumatic regulators, redesigned fuel and LO2 staging valves, and structural changes required to accommodate these differences ...
    Schlagwörter: Vibration , Command and control systems , Control sequences , Pitch(Motion)

    Effect of Lateral-Directional Control Coupling on Pilot Control of an Airplane as Determined in Flight and in a Fixed-Base Flight Simulator

    R. F. Vomaske / M. Sadoff / F. J. Drinkwater | NTIS | 1961
    , indicating that absence of kinesthetic motion cues did not markedly affect the pilots' evaluation of the type of control problem considered in this ...
    Verlag: National Aeronautics and Space Administration, Moffett Field, CA. Ames Research Center
    Schlagwörter: Directional control , Lateral control , Pilot induced oscillation , Aircraft control

    An Approach to the Control of Statically Unstable Manned Flight Vehicles

    M. Dublin | NTIS | 1961
    . Taking a delta wing canard controlled aircraft as an example, this Report presents a control concept based on three redundant systems of ...
    Verlag: Advisory Group for Aeronautical Research and Development Paris (France)
    Schlagwörter: Oscillation , Control systems , Motion

    Forced flexural motion of a rocket-boosted vehicle

    Anderson, R. A. | NTRS | 1962
    Bending vibration equations for rocket boosted vehicle controlled by vectored thrust - structural dynamics ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: BENDING VIBRATION , THRUST VECTOR CONTROL /TVC/

    A Simulator Investigation of a Self-Adaptive Pitch Damper for a High Performance Fighter Aircraft

    D. L. Boslaugh | NTIS | 1962
    variations in airframe transfer function parameters as flight conditions change. Airframe control systems and stability augmentation devices utilized ...
    Schlagwörter: Adaptive control systems , Pitch(Motion) , Equations of motion , Flight control systems

    Report of the Engineering Flight Test -- Stability and Control Phase -- of the OH-4A Helicopter, Unarmed (Clean) and Armed with the XM-7 or XM-8 Weapon Subsystem. Part I

    NTIS | 1964
    Stability and control flight tests were conducted on the OH-4A helicopter to determine the stability and control characteristics throughout ...
    Schlagwörter: Pitch(Motion) , Flight control systems , Vibration

    Report of the Engineering Flight Test -- Performance Phase -- of the OH-4A Helicopter, Unarmed (Clean) and Armed with the XM-7 or XM-8 Weapon Subsystem. Part II

    NTIS | 1964
    Characteristics and to Check the contractual guarantees outlined in the OH-4A Model Specification. ...
    Schlagwörter: Vibration , Flight control systems , Pitch(Motion)

    New Techniques in Packaging

    Hatae, M. T. | SAE Technical Papers | 1964
    for shock and vibration isolation, the trend toward flexible environmental covers, control of temperature during the shipping cycle, and ...

    Airplane vibration -- Practical approach

    Schultz, W.H. | Engineering Index Backfile | 1965
    depend on control and reduction of vibration; designers can generally safeguard against its occurrence by tuning airframe; supplementing design ...

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