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Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls
Author(s): Fenzel, L. R., Nichol, K. C., Wood, L. R.
Corporate Author(s): General Electric Company
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report number: ASD TDR 62-76
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Investigation of Hypersonic Flow Separation and its Effects on Aerodynamic Control Characteristics
Author(s): Abbott, Douglas E., Holt, Maurice, Nielsen, Jack N.
Corporate Author(s): Itek Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-11
Report number: ASD TDR 62-963
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Hypersonic Flow Theories for Predicting Pressures on Blunt Two-Dimensional and on Conical Shapes
Author(s): Scheuing, Richard A., Melnik, Robert E., Brook, John W., Hayes, Wallace D. , Donaldson, Coleman duP. , Sullivan, Rofer D.
Corporate Author(s): Grumman Aircraft Engineering Corporation; Aeronautical Research Associates of Princeton
Laboratory: Flight Control Laboratory
Date of Publication: 1962-06
Report number: ASD TDR 62-167
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Design Techniques and Laboratory Development of an Electrical Primary Flight control System
Author(s): Sethre, V. C., Schenbeck, R. E., Kerber, R. L., Rassi, J. A., Fowler, R. L.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-04
Report number: ASD TDR 62-46
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An Investigation of Magnetohydrodynamic Principles Applicable to Flight Control
Author(s): Ericson, William B., Maciulaitis, Algirdas, Spagnolo, Frank A., Loeffler, Albert L., Scheuing, Richarde A., Hopkins, Harold B.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-12
Report number: ASD TDR 62-649
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Study of Electrically Produced Strain for Control Purposes
Author(s): None Given
Corporate Author(s): Bendix Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-10
Report number: ASD TDR 62-621
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Theoretical Prediction of Pressures in Hypersonic Flow with Special Referencce to Configurations Having Attached Leading Edges Shock: Part II. Experimental Pressure Measurements at Mach 5 and 8
Author(s): Mead, Harold R., Koch, Frank
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TR 61-60 Part 2
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Automatic Landing System Study: Part II. Results of Ground Equipment and Data Transmission Studies
Author(s): Wilkie, R., Smearmon, C., Cope, R.
Corporate Author(s): Bendix Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-02
Report number: ASD TR 61-114 Part II
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Hydraulic Servo Control Valves - Part 8 Valve Performance Evaluation Investigation Of Oil Contamination Effects, And Nuclear Radiation Effects Testing
Author(s): Kinney, Wayne L., Dick, George H.
Corporate Author(s): Cook Technological Center
Laboratory: Flight Control Laboratory
Date of Publication: 1962-10
Report number: WADC TR 55-29 Part 8
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume I Elastic Response Determinations for Severely Heated Wings
Author(s): Gallagher, Richard H., Huff, Rolland D.
Corporate Author(s): Bell Aerosystems Co.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-08
Report number: ASD TR 61-287 Part 2 Volume 1

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