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27 items

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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): Kaufman, Louis G., Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-235
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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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Synthesis of Flight Control Systems Subject to Vehicle Parameter Variations
Author(s): Kreindler, Eliezer
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-04
Report number: AFFDL TR 66-209
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Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity
Author(s): Gilmore, Arthur, Seredinsky, Vladimir, MacKenzie, Donald
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 62-460