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Datcom and the Digital Datcom are in the stability-axis system. Body-axis normal- ... mindful of section characteristics which are sensitive to Reynolds number, particularly in cases where very low Reynolds number estimates are of interest. A
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MISSILE DATCOM User’s Manual - 2011 Revision 5a. CONTRACT NUMBER In-house 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 62201F 6. AUTHOR(S) Christopher Rosema, Joshua Doyle, Lamar Auman, and Mark Underwood (U.S. Army Aviation & Missile Research, Development and Engineering Center) William B. Blake (AFRL/RBCA) 5d. PROJECT NUMBER A07T 5e. TASK ...
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In Brief: Datcom is the United States Air Force Data Compendium, a 3100-page collection of the equations used in design of airplanes. This manual dates back to the 1930’s-1950’s, before computer, when designs and calculations were done by hand and with slide rules.
The DATCOM Manual is divided into 9 sections: Many textbooks utilized in universities implement the DATCOM method of stability and control. Shortly before compilation of the DATCOM was completed, a computerized version called Digital DATCOM was created. The USAF S&C Digital DATCOM implements the DATCOM methods in an easy to use manner.
Digital DATCOM cannot provide outputs for the control derivatives with regard to the rudder control surface. According to the manual, there is no any input parameters which define the geometriy of rudder. Digital DATCOM cannot analyze three lifting surfaces at once, such as a canard-wing-horizontal tail configuration.
Many textbooks utilized in universities implement the DATCOM method of stability and control. Shortly before compilation of the DATCOM was completed, a computerized version called Digital DATCOM was created. The USAF S&C Digital DATCOM implements the DATCOM methods in an easy to use manner. Hoak, D. E., et al.,
Go to the page of references for the Digital Datcom program. Download datcom.zip, containing the source code and sample cases. The archive file datcom.zip contains the files: The 11 sample cases from AFFDL-TR-79-3032 along with the expected output for each.