Accession Number : ADA136182
Title : Development of a Flight Simulation Concept and Aerodynamic Buildup for Investigation of Departure Prevention Systems in Tactical Aircraft.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Raithel,A L , III
Report Date : Sep 1983
Pagination or Media Count : 88
Abstract : The conceptual development of a computer flight simulation for design, testing and analysis of departure prevention systems, simulation capability and programming are discussed, along with required research material and data. A description is given of the aerodynamic buildup program written for incorporation in the simulation, including the aerodynamic equations of the model base aircraft, sample program statements and output.
Descriptors : *Flight simulation , *Computerized simulation , *Flight control systems , *Aerodynamic stability , Tactical aircraft , Models , Computer programming , Simulation , Aerodynamics , Equations , Theses
Subject Categories : Aircraft
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE