Search

27 items

application/pdf thumbnail
full text available
Investigation of Pressure Distributions Over Planar, Twisted, and Cambered Wings in a Hypersonic Shock Tunnel
Author(s): Scheuing, Richard A., Leng, Jarvis
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-05
Report number: ASD TDR 62-171
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
The Calculation of Nonlinear Supersonice Conical Flows by the Method of Integral Relations
Author(s): Brook, John W.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report number: FDL TDR 64-7
application/pdf thumbnail
full text available
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
application/pdf thumbnail
full text available
A Review of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., Oman, Richard A., Hartofilis, Stavros A., Meckler, Lawrence H., Evans, William J., Weiss, Daniel
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1962-03
Report number: ASD TDR 62-168
full text unavailable
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
full text unavailable
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