DATCOM MANUAL PDF

The United States Air Force Stability and Control DATCOM is a collection, correlation, codification, and recording of best knowledge, opinion, and judgment in the area of aerodynamic stability and control prediction methods. It presents substantiated techniques for use 1 early in the design or concept study phase, 2 to evaluate changes resulting from proposed engineering fixes, and 3 as a training on crosstraining aid. It bridges the gap between theory and practice by including a combination of pertinent discussion and proven practical methods. For any given configuration and flight condition, a complete set of stability and control derivatives can be determined without resort to outside information. A spectrum of methods is presented, ranging from very simple and easily applied techniques to quite accurate and thorough procedures.

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National Technical Reports Library. Session Timeout. Your session has time out. Volume I. Users Manual. Page Count Abstract 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 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 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.

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 Corporate Authors. McDonnell Douglas Astronautics Co. Louis, MO. Supplemental Notes. Supersedes Rept. See also Volume 2, AD-A Publication Date. Personal Author. Williams, J. Page Count. Source Agency.

Document Type. Technical Report. Title Note. Final rept. Aug Nov Contract Number.

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USAF Stability and Control DATCOM

National Technical Reports Library. Session Timeout. Your session has time out. Volume I. Users Manual. Page Count Abstract 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 Configuration geometry, attitude, and Mach range capabilities are consistent with those accommodated by the Datcom.

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National Technical Reports Library

Skip to search form Skip to main content You are currently offline. Some features of the site may not work correctly. Corpus ID: Missile Datcom. Bruns and Marvin E. Moore and Stan L. Stoy and Steven R. Vukelich and William B.

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