MACH NUMBER INDEPENDENT HOT-WIRE ANEMOMETRY
Abstract
The proposed research program aims to produce a new generation of probes specifically designed for high-speed flow anemometry based on the nano-scale thermal anemometry probe (NSTAP) recently developed at Princeton’s University. They will be validated by laminar, transitional, and turbulent supersonic wind-tunnel measurements. Associated to new electronic devices, these probes will provide an unprecedented level of accuracy, bandwidth and dynamic range.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Aug 11, 2021
- Source ID
- FA86552017040
Entities
People
- Pierre Dupont
Organizations
- Air Force Office of Scientific Research
- United States Air Force