Accession Number : ADA136376
Title : Computer Programs for Helicopter High Speed Flight Analysis.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Carmona,W F
PDF Url : ADA136376
Report Date : Sep 1983
Pagination or Media Count : 139
Abstract : This report gives to the user of the HP41-CV handheld programmable calculator or the IBM 3033 computer a blade element method for calculating the total power required in forward, straight and level high-speed flight for an isolated rotor. The computer programs consist of a main program which calculates the necessary dynamic parameters of the main rotor and several subroutines which calculate power required as well as maximum forward velocity, stall onset velocity, and velocity for best endurance.
Descriptors : *Rotor blades(Rotary wings), *Stalling, Computer programs, Aerodynamics, Helicopter rotors, Flight paths, High velocity, Helicopters, Level flight, Angle of attack, Compressive properties, Digital simulation, man computer interface, Computer aided design, Power, Parametric analysis, Subroutines, Endurance(General), Digital computers, Computer program documentation, Theses
Subject Categories : Helicopters
Computer Programming and Software
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE