12 reports
Pressure and Heat Transfer Measurements at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics
Author(s): Louis G. Kaufman; Lawrence Meckler Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Flight Control Laboratory Date of Publication: 1963-04 Report Number: ASD TDR 63-235
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Thermoelastic Effects on Hypersonic Stability and Control: Part III: Hypersonic Aeroelasticity
Author(s): Joseph Padlog; Vincent W. Donato; James R. Batt Corporate Author: Bell Aerosystems Company Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TR 61-287 Part 3
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A Study of Time-Based Methods of Analysis in Cockpit Design
Author(s): Lewis F. Hanes; Malcolm L. Ritchie; John H. Kearns Corporate Author: Ritchie and Associates; Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TDR 63-289
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Thermoelastic Effects on Hypersonic Stability and Control Part I. Hypersonic Aerodynamics
Author(s): None Given Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TR 61-287 Part 1
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Performance Criteria for Linear Constant-Coefficient Systems with Random Inputs
Author(s): Raymond Magdaleno and Julian Wolkovitch Corporate Author: Systems Technology, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1963-01 Report Number: ASD TDR 62-470
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A Study of Selected Contorl-Display Problems for Manned Aerospace Vehicles
Author(s): Pickel, Francis E. Corporate Author: Lear, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1963-03 Report Number: ASD TDR 63-170
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Altimeter Display and Hardware Development 1903-1960
Author(s): Schum, David A. Corporate Author: Bell Helicopter Company Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TDR 63-288
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Engineering Analysis Methods for Linear Time Varying Systems
Author(s): Graham, Dunstan Corporate Author: Systems Technology, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1963-01 Report Number: ASD TDR 62-362
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Control System Redundancy Mechanization Study
Author(s): Tesch, E. Corporate Author: Minneapolis-Honeywell Regulator Company Laboratory: Flight Control Laboratory Date of Publication: 1963-02 Report Number: ASD TDR 62-772
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Experimental Investigation of Pressures on a Blunt Two-Dimensional Profile and on Sharp and Blunt Conical Shapes of Noncircular Cross Section at Mach 5 and 8
Author(s): Mead, Harold R. Corporate Author: Grumman Aircraft Engineering Corporation Laboratory: Flight Control Laboratory Date of Publication: 1963-08 Report Number: ASD TDR 63-169
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume III: Elastic Response Analysis of Fuselage and Combined Wing-Fuselage Structures
Author(s): Huff, Rolland D. Corporate Author: Bell Aerosystems Company Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TR 61-287 Part 2 Volume 3
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume II: Elevated Temperature Deflection Influence Coefficient Tests
Author(s): Quinn, James F. Corporate Author: Bell Aerosystems Company Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TR 61-287 Part 2 Volume 2
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