Evolution and Stability of Vortical Gusts Impinging Upon Elastic Wings
Abstract
The objective of the proposed effort is to gain fundamental insight into the dynamics, distortion, and stability of finite-core, rectilinear vortices and their interactions with an elastic wing through the development of mathematical models. These models will then be used to study the evolution of vortices produced by leader aircraft and their coupled interactions with the wings of follower aircraft in formation flight.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501510148
Entities
People
- Justin Jawarski
Organizations
- Air Force Office of Scientific Research
- Lehigh University
- United States Air Force