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Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Evans, William J., Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-128
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A Conical Thin-Shock-Layer Theory Uniformly Valid in the Entropy Layer
Author(s): Melnik, Robert E.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: FDL TDR 64-82
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Pressure and Heat Transfer Measurements at Mach 13 and 19 for Flows Ahead of Ramps, Over Expansion Corners, and Past Fin-Plate Combinations: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hatofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-144
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part II" Pressure Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-2 Part 2
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Statistical Control System Design
Author(s): Reiss, R., Mendelsohn, J., Van Gelder, A., Taylor, G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-10
Report number: AFFDL TR 66-83
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Matrix Analysis Methods for Inelastic Structures
Author(s): Lansing, W., Jensen, W. R., Falby, W.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 603-633
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Fully-Stressed Design of Airplane Redundant Structures
Author(s): Dwyer, W., Shulman, M., Pardo, H., Rosenbaum, J.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 155-181
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A Finite Element Method for the Plastic Bending Analysis of Structures
Author(s): Armen, A., Jr., Levine, H. S., Pifko, A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 1301-1339

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