NASA NTRS · 19730010555
Numerical calculations of flow fields
Abstract
Numerical calculations were made of flow fields generated by various aerodynamic configurations. Data cover flow fields generated by a finitely thick lifting three dimensional wing with subsonic tips moving at supersonic speeds, cross flow instability associated with lifting delta wing configurations such as space shuttles, and flow fields produced by a lifting elliptic cone. Finite difference techniques were used to determine elliptic cone flow.
Keep this discovery
Explore connections, maps & timelines
Anderson, D., Vogel, J. M.. 1973-01-01. Numerical calculations of flow fields. https://ntrs.nasa.gov/citations/19730010555
Cite the original work for its findings. Save a collection to share your selection of sources.