Numerical analysis of high speed wind tunnel flow disturbance measurements using stagnation point probes

DOI10.1017/jfm.2017.674zbMath1419.76550OpenAlexW2766660061MaRDI QIDQ5225998

Thomas Schilden, Wolfgang Schröder

Publication date: 30 July 2019

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2017.674

zbMATH Keywords

shock wavesgas dynamicshigh-speed flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Gas dynamics (general theory) (76N15) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (2)

Algorithmic differentiation of hyperbolic flow problems ⋮ Inclined slow acoustic waves incident to stagnation point probes in supersonic flow

Cites Work

• Unnamed Item
• Unnamed Item
• Unnamed Item
• An adaptive multilevel multigrid formulation for Cartesian hierarchical grid methods
• Massively parallel grid generation on HPC systems
• Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
• Note on the Assessment of Flow Disturbances at a Blunt Body Traveling at Supersonic Speeds Owing to Flow Disturbances in Free Stream
• Receptivity of a high-speed boundary layer to acoustic disturbances
• Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
• Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
• Transition and Stability of High-Speed Boundary Layers
• Receptivity of a high-speed boundary layer to temperature spottiness
• Interaction of Linear Waves with Oblique Shock Waves
• Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances

This page was built for publication: Numerical analysis of high speed wind tunnel flow disturbance measurements using stagnation point probes