| タイトル | LinAir: A multi-element discrete vortex Weissinger aerodynamic prediction method |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940019084 |
| 著者（英） | Durston, Donald A. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1993-10-01 |
| 言語 | eng |
| 内容記述 | LinAir is a vortex lattice aerodynamic prediction method similar to Weissinger's extended lifting-line theory, except that the circulation around a wing is represented by discrete horseshoe vortices, not a continuous distribution of vorticity. The program calculates subsonic longitudinal and lateral/directional aerodynamic forces and moments for arbitrary aircraft geometries. It was originally written by Dr. Ilan Kroo of Stanford University, and subsequently modified by the author to simplify modeling of complex configurations. The Polhamus leading-edge suction analogy was added by the author to extend the range of applicability of LinAir to low aspect ratio (i.e., fighter-type) configurations. A brief discussion of the theory of LinAir is presented, and details on how to run the program are given along with some comparisons with experimental data to validate the code. Example input and output files are given in the appendices to aid in understanding the program and its use. This version of LinAir runs in the VAX/VMS, Cray UNICOS, and Silicon Graphics Iris workstation environments at the time of this writing. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 94N23557
NASA-TM-108786
A-93111
NAS 1.15:108786 |
| 権利 | No Copyright |
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