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. (Author)
STOL Tactical Aircraft Investigation. Volume II. Part I. Aerodynamic Technology: Design Compendium, Vectored Thrust/Mechanical Flaps
1973
234 pages
Report
No indication
English