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Helicopter rotor loads using matched asymptotic expansions: user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Vaidyanathan, A. R. Pierce, G. A. |
| Copyright Year | 1983 |
| Description | Computer programs were developed to implement the computational scheme arising from Van Holten's asymptotic method for calculating airloads on a helicopter rotor blade in forward flight, and a similar technique which is based on a discretized version of the method. The basic outlines of the two programs are presented, followed by separate descriptions of the input requirements and output format. Two examples illustrating job entry with appropriate input data and corresponding output are included. Appendices contain a sample table of lift coefficient data for the NACA 0012 air foil and listings of the two programs. |
| File Size | 2584579 |
| Page Count | 94 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830017388 |
| Archival Resource Key | ark:/13960/t2m66bj31 |
| Language | English |
| Publisher Date | 1983-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Horizontal Flight Incompressible Flow Computational Fluid Dynamics Rotor Aerodynamics Discrete Functions Wing Loading Asymptotic Methods User Manuals Computer Programs Rotary Wings Potential Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
