Academic Journal

General Description of the Rotorcraft Flight Simulation Computer Program (G-81)

Bibliographic Details
Title: General Description of the Rotorcraft Flight Simulation Computer Program (G-81)
Authors: Austin, Edward E., Vann, William D.
Contributors: ARMY AIR MOBILITY RESEARCH AND DEVELOPMENT LAB FORT EUSTIS VA EUSTIS DIRECTORATE
Source: DTIC AND NTIS
Publication Year: 1973
Collection: Defense Technical Information Center: DTIC Technical Reports database
Subject Terms: Aerodynamics, Helicopters, HELICOPTERS, MATHEMATICAL MODELS, SIMULATION, STABILITY, AIRFRAMES, AERODYNAMIC CONTROL SURFACES, AERODYNAMIC CHARACTERISTICS, COMPUTER PROGRAMMING, ROTOR BLADES(ROTARY WINGS), SIX DEGREES OF FREEDOM, DIGITAL SIMULATION
Description: The rotorcraft flight simulation is a multidisciplinary mathematical model that may be used to simulate a wide variety of helicopter or V/STOL aircraft configurations using a digital computer. Aircraft performance, stability and control, and maneuver characteristics, as well as rotor blade loads, may be estimated using this analysis. The fuselage, main rotor, tail rotor, wing, elevator, fin/rudder, jet thrust, and weapon recoil are treated as separate aircraft components, allowing detailed representation of the aircraft for design or detailed analysis applications. Six rigid-body fuselage degrees of freedom and up to six rotor blade elastic degrees of freedom for each of two rotors are accounted for. Input for the simulation is divided into logical blocks in an easy-to-understand format. The rotor blade elastic degrees of freedom are omitted if stiffness and mass properties are not known. Output includes aircraft trim attitude, control positions, performance rotor loads, stability and control characteristics, and detailed maneuver response.
Document Type: text
File Description: text/html
Language: English
Relation: http://www.dtic.mil/docs/citations/AD0767239
Availability: http://www.dtic.mil/docs/citations/AD0767239
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0767239
Rights: Approved for public release; distribution is unlimited.
Accession Number: edsbas.FC55AA64
Database: BASE
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