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The Effects Of Engine Angular Momentum On An Airplane's Longitudinal And Lateral-Directional Dynamic Stability
Author(s): Paiewonsky, Bernard H.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-225
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Magnetic Servo Amplifliers For Flight Control Systems
Author(s): Frank, Max, Walker, J. R.Corporate Author(s): Wayne Engineering Research Institute, Wayne University
Laboratory: Flight Control Laboratory
Date of Publication: 1956-10
Report number: WADC TR 56-271
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Methods For Estimating Aeroelastic Effects On Subsonic Lateral-directional Stability Derivitives Of Aircraft
Author(s): Cahen, George L., Preyss, Albert E.Corporate Author(s): Glenn L. Martin Company
Laboratory: Flight Control Laboratory
Date of Publication: 1956-10
Report number: WADC TR 56-345
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The Effects Of Structural Elasticity On Aircraft Control Systems
Author(s): Howard, Vincent W.Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Flight Control Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-166
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part III. The Coordinated Design Of Magnetic Amplifiers And Motors
Author(s): Perrins, Allen R.Corporate Author(s): Yale University
Laboratory: Flight Control Laboratory
Date of Publication: 1956-05
Report number: WADC TR 56-199 Part 3
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part IV. Diverse Topics: Magnetic Frequency Multipliers, Two Phase Servo, Relay Servo, Input Circuits, Coupling Networks
Author(s): Barker, R. C., Wakeman, C. B., Perrins, A. R.Corporate Author(s): Yale University
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TR 56-199 Part 4
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part V. Summary And Recommendations
Author(s): Barker, Richard ClarkCorporate Author(s): Yale University
Laboratory: Flight Control Laboratory
Date of Publication: 1956-12
Report number: WADC TR 56-199 Part 5
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Boundary Layer Control Applied To Tail Surfaces Of A Aircraft . Part II: Final Report
Author(s): Gersten, W. M., Wise, W. D.Corporate Author(s): Cessna Aircraft Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-12
Report number: WADC TR 57-741 Part 2
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Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report
Author(s): Leisher, L. L., Gertsen, W. M.Corporate Author(s): Cessna Aircraft Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-12
Report number: WADC TR 57-741 Part 1
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Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft
Author(s): Van Meter, J. T., McLane, R. C.Corporate Author(s): Minneapolis-Honeywell Regulator Company
Laboratory: Flight Control Laboratory
Date of Publication: 1957-06
Report number: WADC TR 57-349
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