NASA NTRS · 19820000064
Higher-Order Panel Method for Aerodynamic Flow Analysis
Abstract
PANAIR uses high-order panel method to predict inviscid subsonic or supersonic flows about arbitrary configuration. Panel method solves linear partial differential equation numerically by approximating configuration surface with panels on which unknown "singularity strengths" are defined. PANAIR includes advanced software technology as well as advanced aerodynamic technology.
Keep this discovery
Explore connections, maps & timelines
Erickson, L., Carmichael, R. L., Levin, A. D., Magnus, A., Epton, M., Baruah, P., Massena, B., Bussoletti, J., Sidwell, K., Johnson, F., Zeppa, J., Bates, G., Clemens, D., Derbyshire, T., Purdon, D., Chiang, D., Rubbert, P., Nelson, F., Wai, J., Tsurusaki, K., Smith, N., Snyder, J. R., Sotomayer, W., Dejongh, J., Thomas, J. L.. 1982-12-01. Higher-Order Panel Method for Aerodynamic Flow Analysis. https://ntrs.nasa.gov/citations/19820000064
Cite the original work for its findings. Save a collection to share your selection of sources.