Lecture
Supersonic Wind Tunnel - EPFL Rocket Team
In course
DEMO: cillum et
In duis irure eu eu dolor sit in sint. Deserunt adipisicing tempor ut eu. Anim consequat reprehenderit nostrud nulla ex aliqua laborum irure aute cupidatat exercitation et aliquip amet. Occaecat ea nostrud labore mollit sit cupidatat qui pariatur tempor eiusmod. Ut sint non id culpa dolor Lorem culpa consequat consequat. Ex officia laborum culpa deserunt cupidatat non pariatur ipsum laboris.
Description
This lecture presents a project conducted in collaboration with the EPFL Rocket Team to visualize supersonic flows on HL-R8 models using the Schlieren method, aiming to optimize rocket design for supersonic flight.
Official source
About this result
This page is automatically generated and may contain information that is not correct, complete, up-to-date, or relevant to your search query. The same applies to every other page on this website. Please make sure to verify the information with EPFL's official sources.
Ontological neighbourhood
Related lectures (34)
Convergent-Divergent Nozzles
Explores the performance advantages of convergent-divergent nozzles in supersonic applications.
Shock and Expansion Waves: Animations
Explores shock and expansion waves through animations, demonstrating their effects on air density and refractive index.
Straight Shocks: Entropy
Explores straight shocks in fluid dynamics, discussing entropy, ideal gases, and the Rankine-Hugoniot relation.
Isentropic Flows and Mach Waves
Covers isentropic flows, Mach waves, and their interaction in supersonic flows.
Variable Mass System and Accelerated Frames
Explores variable mass systems, rocket thrust, takeoff conditions, and accelerated frames.