Mathematical Modeling and Control of Wind Tunnels for the Investigation of Low Reynolds-Number, Unsteady Aerodynamic Effects
Abstract
The primary objective of the proposed effort is to investigate improved methods for accurate and rapid control of the test wind speed in wind tunnels for the purpose of investigating low-Re, unsteady-aerodynamic effects.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Mar 23, 2016
- Source ID
- FA95501610067
Entities
People
- Robert Rennie
Organizations
- Air Force Office of Scientific Research
- United States Air Force
- University of Notre Dame