NASA NTRS · 19730004563
Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings: User's manual
Abstract
The input data required to execute the computer program AIC/INT (aerodynamic influence coefficients with interference) are presented. The purpose of the computer program is to generate aerodynamic forces for a pair of plane and interfering nearly parallel, non-coplanar wings at supersonic Mach numbers. A finite element technique has been employed. Planforms are described by triangular elements and diaphragm regions are generated automatically.
Keep this discovery
Explore connections, maps & timelines
Paine, A. A.. 1972-08-01. Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wings: User's manual. https://ntrs.nasa.gov/citations/19730004563
Cite the original work for its findings. Save a collection to share your selection of sources.