NDLI: Aeroelastic analysis for propellers - mathematical formulations and program user's manual

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Aeroelastic analysis for propellers - mathematical formulations and program user's manual

Content Provider	NASA Technical Reports Server (NTRS)
Author	Gangwani, S. T. Chi, R. M. Johnson, S. A. Bielawa, R. L.
Copyright Year	1983
Description	Mathematical development is presented for a specialized propeller dedicated version of the G400 rotor aeroelastic analysis. The G400PROP analysis simulates aeroelastic characteristics particular to propellers such as structural sweep, aerodynamic sweep and high subsonic unsteady airloads (both stalled and unstalled). Formulations are presented for these expanded propeller related methodologies. Results of limited application of the analysis to realistic blade configurations and operating conditions which include stable and unstable stall flutter test conditions are given. Sections included for enhanced program user efficiency and expanded utilization include descriptions of: (1) the structuring of the G400PROP FORTRAN coding; (2) the required input data; and (3) the output results. General information to facilitate operation and improve efficiency is also provided.
File Size	8743421
Page Count	254
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19840004462
Archival Resource Key	ark:/13960/t2g78720x
Language	English
Publisher Date	1983-12-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Propellers Subsonic Flow Sweep Effect Rotor Aerodynamics Mathematical Models Computerized Simulation Flutter Analysis Unsteady Flow Aeroelasticity Aerodynamic Stalling User Manuals Computer Programs Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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