DYNAMIC RESPONSE ON THE SHEAR LAYER TO CAVITY DOOR OPERATION AT SUPERSONIC SPEEDS
Abstract
The proposed work will result in a better understanding of the flow physics associated with moving aerodynamic surfaces in supersonic flow in general, and more specifically on how aerodynamic feedback geometries, such as cavities, are affected under these circumstances. This integrated study will significantly leverage the established expertise of the investigators, especially in the areas of experimental aerodynamics and high-fidelity numerical simulations, while taking advantage of the existing facilities and computational resources. Consequently, the students engaged in this research and its outcomes will come from a unique, culturally diverse population. This project will benefit the goal of producing African-American graduate degrees in engineering and supporting future faculty. The results will be broadly disseminated through presentations at professional meetings, publication in journals, and through the investigators’ very active collaborations with scientists at defense research laboratories, especially those within the Air Force Research Laboratories.
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Aug 12, 2021
- Source ID
- FA95502010199
Entities
People
- Kumar Rajan
Organizations
- Air Force Office of Scientific Research
- Florida A&M University
- United States Air Force