- Author : National Aeronautics and Space Administration (NASA)
- Publisher : Createspace Independent Publishing Platform
- Release : 2018-07-09
- ISBN : 9781722407025
- Pages : 32 pages
Navier Stokes and Potential Theory Solutions for Ahelicopter Fuselage and Comparison with Experiment
Download or read book Navier Stokes and Potential Theory Solutions for Ahelicopter Fuselage and Comparison with Experiment written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-09 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: A thin-layer Navier-Stokes code and a panel method code are used to predict the flow over a generic helicopter fuselage. The computational results are compared with pressure data at four experimental conditions. Both methods produce results that agree with the experimental pressure data. However, separation patterns and other viscous flow features from the Navier-Stokes code solution are shown that cannot be easily modeled with the panel method. Chaffin, Mark S. and Berry, John D. Langley Research Center NAS1-19672; RTOP 505-59-36-01; RTOP 023-10-01-01...