WebHIFiRE-5 is the second of two flights in the HIFiRE manifest focused on boundary layer transition. The HIFiRE-1 program created an extensive knowledge base regarding … WebThe HIFiRE-5 transition experiment extends the HIFiRE-1 effort to fully three-dimensional boundary layers, by seeking to transition locations around the body of a non-ablating, 2:1 elliptic cone. The experiment is designed to generate both crossflow and second-mode transition. The primary goal behind the current work is to generate design data ...
HIFiRE program DST - Department of Defence
Web22 de mai. de 2016 · Published on May 18, 2016. Experimental rocket HiFiRE 5B was launched from the Woomera Test Range in South Australia, achieved the targeted speed of Mach 7.5 (seven and a half times the speed of sound, approximately 9200 km/h) and reached a height of 278 kilometres from Earth. Hypersonic International Flight Research … Web1 de mar. de 2024 · HIFiRE 5b Heat Flux and Boundary Layer Transition. DTIC Science & Technology. 2024-11-14. contain a detailed description of the HIFiRE-5 configuration.The HIFiRE-5 vehicle is an elliptic cone with a 2:1 aspect ratio.It has a 7-degree half... description of the HIFiRE-5b vehicle and launch.Figure 1 presents a dimensioned … trymer alpha atp-05
HIFiRE-5 Flight Test Results Request PDF - ResearchGate
Web28 de jun. de 2010 · HIFiRE flight 5 is devoted to measuring transition on a three-dimensional body. This paper summarizes payload configuration, trajectory, vehicle … WebSelected results pertaining to both second mode and crossflow instability over the HIFiRE-1 configuration are presented in sections 2 and 3, respectively. Analogous results for a subscale wind tunnel model of the HIFiRE-5 flight configuration are presented in Section 4. 2. HIFiRE-1 Transition Analysis during Ascent Phase WebHIFiRE is one of the largest (US $54 million) collaborative research programs between Australia and the USA. It aims to explore the fundamental science of hypersonics and … trymer alpha atp-01