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aircraft-datcom is a modified version of USAF Aircraft DATCOM The goal of the project is to update the code and make it more usable by the end users PR: 207928 Submitted by: Michael Danilov <mike.d.ft402@gmail.com>
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716 B
Plaintext
16 lines
716 B
Plaintext
This computer program calculates static stability, high lift and control, and
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dynamic derivative characteristics using the methods contained in the USAF
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Stability and Control Datcom (Data Compendium). Configuration geometry,
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attitude, and Mach range capabilities are consistent with those accommodated by
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the Datcom. The program contains a trim option that computes control
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deflections and aerodynamic increments for vehicle trim at subsonic Mach
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numbers.
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WWW: http://www.pdas.com/datcom.html
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This project is a modified version of the publically released USAF aircraft
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datcom. The goal of the project is to update the code and make it more usable
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by the end user.
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WWW: https://github.com/arktools/aircraft-datcom
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