STOL Tactical Aircraft Investigation. Volume 2. Part 1. Aerodynamic Technology: Design Compendium, Vectored Thrust/Mechanical Flaps
Final technical rept. 8 Jun 1971-8 Dec 1972
BOEING AEROSPACE CO SEATTLE WA
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The report presents methods for predicting the performance determining aerodynamic characteristics and the stability derivatives of transport-type configurations employing the vectored-thrust mechanical-flap high-lift concept. These methods are suitable for preliminary design. They have been automated in a FORTRAN 4 computer program, for which a users manual and listing are included in this document.