DURIP Hypersonic Aerothermodynamics, High-Speed Propulsion and Materials
Abstract
ABSTRACT 1ABSTRACTProgram Officer: Dr. Eric Marineau, ONRHypersonic Aerothermodynamics, High-Speed Propulsion and MaterialsThe acquisition of new experimental hardware is proposed in support of ongoing ONR-fundedresearch into the development and application of spectrally resolved laser diagnostics for propulsionsystems and hypersonic flows. This proposal is structured as two distinct hardwarerequests addressingeach of these topic areas.Request 1: Advanced Laser Diagnostics for Solid Fuel Ramjet FlowsThe request includes the necessary hardware to develop, construct, and implement a bespoke high-bandwidth TDLAS system to characterize model combustor inlet and exhaust flows with sufficientdetail to enable improvements in fundamental combustor flow models presently under development.Request 2: Optically Accessible Nozzles for the Development of Hypersonic Flow DiagnosticsThis request includes optically accessiblenozzles for the new Stanford Reflected Shock Tunnelpresently under construction. This tunnel is designed to generate hypersonic flows with a strongemphasis placed on facilitating the development of advanced laser diagnostic capabilities that may bereadily transitioned to national-scale hypersonic flow facilities at other academic and governmentresearch centers.[Approved for public release]
Document Details
- Document Type
- DoD Grant Award
- Publication Date
- Nov 09, 2024
- Source ID
- N000142412576
Entities
People
- Ronald Kent Hanson
Organizations
- Office of Naval Research
- Stanford University
- United States Navy