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


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a136182.pdf


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