Accession Number : AD0770449
Title : STOL Tactical Aircraft Investigation-Externally Blown Flap. Volume V. Flight Control Technology. Part II. Simulation Studies/Flight Control System Validation.
Descriptive Note : Final rept. 10 Jun 71-10 Dec 72,
Corporate Author : ROCKWELL INTERNATIONAL CORP LOS ANGELES CALIF LOS ANGELES AIRCRAFT DIV
Personal Author(s) : Campbell,James E. ; Elsanker,William K. ; Okumoto,Victor H.
Report Date : APR 1973
Pagination or Media Count : 210
Abstract : The basic objective of the work reported was to provide a broader technology base to support the development of a medium STOL Transport (MST) airplane. This work was limited to the application of the externally blown flap (EBF) powered lift concept. From an overall assessment of study results, it is concluded that the EBF concept provides a practical means of obtaining STOL performance for an MST with relatively low risk. (Modified author abstract)
Descriptors : *Flight control systems, *Short takeoff aircraft, Flaps(Control surfaces), Aeronautics, Flight simulation, Mathematical models, Computerized simulation
Subject Categories : V/STOL
Distribution Statement : APPROVED FOR PUBLIC RELEASE