Accession Number : ADA012028
Title : V/STOL Employing ARL Thrust Augmentation Concepts - Research Test Vehicle Configuration Summary and Design Technology Report.
Descriptive Note : Technical rept. 17 Jul 67-17 Dec 68,
Corporate Author : BELL AEROSPACE CO BUFFALO N Y
Personal Author(s) : Henderson,C.
Report Date : DEC 1968
Pagination or Media Count : 434
Abstract : The results of a detailed preliminary design study of a V/STOL research test vehicle (RTV), employing ARL thrust augmentation concepts, are presented. The V/STOL research airplane uses a high by-pass ratio turbofan engine with ejector thrust augmentation in the wing and fuselage nose. Design layouts of all major configuration components and systems are presented together with results of analytical investigations and trade-off studies.
Descriptors : *Vertical takeoff aircraft, *Short takeoff aircraft, *Thrust augmentation, Turbofan engines, Bypass engines, Ejectors, Configuration, Flight control systems
Subject Categories : V/STOL
Distribution Statement : APPROVED FOR PUBLIC RELEASE