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

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

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

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

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

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

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

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

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

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

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

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