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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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A Method for Estimating Damping Derivatives of VTOL Aircraft in Transition and Hovering Flight
Author(s): Paiewonsky, Bernard H.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-410
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Investigation of a Technique for Improving Aircraft Response Using a Complementary Optimum-Response Model
Author(s): Rath, Raymond R.Corporate Author(s): Flight Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1956-09
Report number: WADC TN 56-475
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Approximate Airframe Transfer Functions And Application To A Single Sensor Control Systems
Author(s): Ashkenas, Irving L., McRuer, Duane T.Corporate Author(s): Kelsey-Hayes Co.
Laboratory: Flight Control Laboratory
Date of Publication: 1958-06
Report number: WADC TR 58-82
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An Analytical Study Of The Dynamics Of Spinning Aircraft. Part 1. Flight Test Data Analyses And Spin Claculations
Author(s): Wykes, John H., Casteel, Gilbert R., Collins, Richard A.Corporate Author(s): North American Aviation, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1958-12
Report number: WADC TR 58-381 Part 1
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