The Usaf Stability And Control Digital Datcom
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Author | : John E. Williams |
Publisher | : |
Total Pages | : 320 |
Release | : 1979 |
Genre | : Space vehicles |
ISBN | : |
File characteristics: Software; 400 files on diskette; ASCII character set; 2 diskettes; Physical description: 3 1/2 diskette high density; System requirements: Mainframe or workstation; VMS; Fortran computer, 3MB of storage. A digital computer program which calculates static stability, high lift and control and dynamics derivative characteristics using the methods contained in the USAF Stability and Control Datcom (rev. Apr 76).
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 1979 |
Genre | : |
ISBN | : |
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in the USAF Stability and Control Datcom (revised April 1976). Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume I is the user's manual and presents program capabilities, input and output characteristics, and example problems. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author | : McDonnell Douglas Astronautics Company-St. Louis |
Publisher | : |
Total Pages | : |
Release | : 1976 |
Genre | : |
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Author | : John E. Williams |
Publisher | : |
Total Pages | : 86 |
Release | : 1979 |
Genre | : Space vehicles |
ISBN | : |
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in the USAF Stability and Control Datcom. Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume III discusses a separate plot module for Digital Datcom. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author | : John E. Williams |
Publisher | : |
Total Pages | : 317 |
Release | : 1979 |
Genre | : |
ISBN | : |
Volume I is the user's manual and presents program capabilities, input and output characteristics, and example problems. Volume II describes program implementation of Datcom methods. Volume III discusses a separate plot module for Digital Datcom.
Author | : |
Publisher | : |
Total Pages | : 78 |
Release | : 1979 |
Genre | : |
ISBN | : |
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in the USAF Stability and Control Datcom. Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume III discusses a separate plot module for Digital Datcom. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author | : John E. Williams |
Publisher | : |
Total Pages | : 552 |
Release | : 1977 |
Genre | : Space vehicles |
ISBN | : |
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in sections 4 through 7 of the USAF Stability and Control Datcom (revised January 1974). Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume II describes program implementation of Datacom methods. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author | : |
Publisher | : |
Total Pages | : 161 |
Release | : 1979 |
Genre | : |
ISBN | : |
This report describes a digital computer program that calculates static stability, high lift and control, and dynamic derivative characteristics using the methods contained in the USAF Stability and Control Datcom. Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom. The program contains a trim option that computes control deflections and aerodynamic increments for vehicle trim at subsonic Mach numbers. Volume II describes program implementation of Datcom methods. The program is written in ANSI Fortran IV. The primary deviations from standard Fortran are Namelist input and certain statements required by the CDC compilers. Core requirements have been minimized by data packing and the use of overlays. User oriented features of the program include minimized input requirements, input error analysis, and various options for application flexibility.
Author | : Douglas Aircraft Company |
Publisher | : |
Total Pages | : |
Release | : 1965 |
Genre | : Stability of airplanes |
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Author | : |
Publisher | : |
Total Pages | : |
Release | : 1968 |
Genre | : |
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