NASA NTRS · 19810010564
GASP- General Aviation Synthesis Program. Volume 3: Aerodynamics
Abstract
Aerodynamics calculations are treated in routines which concern moments as they vary with flight conditions and attitude. The subroutines discussed: (1) compute component equivalent flat plate and wetted areas and profile drag; (2) print and plot low and high speed drag polars; (3) determine life coefficient or angle of attack; (4) determine drag coefficient; (5) determine maximum lift coefficient and drag increment for various flap types and flap settings; and (6) determine required lift coefficient and drag coefficient in cruise flight.
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Hague, D.. 1978-01-01. GASP- General Aviation Synthesis Program. Volume 3: Aerodynamics. https://ntrs.nasa.gov/citations/19810010564
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