NASA NTRS · 19910000209
Calculation Of Aeroelastic Transients Using Euler Equations
Abstract
Method for calculation of transient aeroelastic effects on airplane wings based on Euler equations of flow. Conforming grids facilitate calculations of flows about changing shapes. Capability to compute aeroelastic effects reduces cost of developing aircraft.
Keep this discovery
Explore connections, maps & timelines
Guruswamy, Guru P.. 1991-05-01. Calculation Of Aeroelastic Transients Using Euler Equations. https://ntrs.nasa.gov/citations/19910000209
Cite the original work for its findings. Save a collection to share your selection of sources.