NASA NTRS · 19810010566
GASP- General Aviation Synthesis Program. Volume 5: Weight
Abstract
Subroutines for determining the weights of propulsion system related components and the airframe components of an aircraft configuration are presented. Subroutines that deal with design load conditions, aircraft balance, and tail sizing are included. Options for turbine and internal combustion engines are provided.
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Hague, D.. 1978-01-01. GASP- General Aviation Synthesis Program. Volume 5: Weight. https://ntrs.nasa.gov/citations/19810010566
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