Secondary instability analysis of crossflow on a hypersonic yawed straight circular cone
From MaRDI portal
Publication:5364435
DOI10.1017/jfm.2016.793zbMath1383.76242OpenAlexW2566617410MaRDI QIDQ5364435
Helen L. Reed, Pedro Paredes, Alexander J. Moyes, Travis S. Kocian
Publication date: 28 September 2017
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2016.793
Related Items (4)
Boundary layer transition and linear modal instabilities of hypersonic flow over a lifting body ⋮ Cross-flow vortices and their secondary instabilities in hypersonic and high-enthalpy boundary layers ⋮ Crossflow instability in a hypersonic boundary layer ⋮ The secondary instabilities of stationary cross-flow vortices in a Mach 6 swept wing flow
Cites Work
- Unnamed Item
- Unnamed Item
- Spatially developing secondary instabilities in compressible swept airfoil boundary layers
- Control of flow instabilities and unsteady flows
- Secondary instability of crossflow vortices: validation of the stability theory by direct numerical simulation
- Stability of the Boundary Layer on a Swept Wing with Wall Cooling Spyridon
- Stability of three-dimensional supersonic boundary layers
- Primary and secondary stability analysis of a three-dimensional boundary-layer flow
- On a degeneracy of temporal secondary instability modes in Blasius boundary-layer flow
- Short Lecture Sessions
- Crossflow disturbances in three-dimensional boundary layers: nonlinear development, wave interaction and secondary instability
- S<scp>TABILITY AND</scp> T<scp>RANSITION OF</scp> T<scp>HREE</scp>-D<scp>IMENSIONAL</scp> B<scp>OUNDARY</scp> L<scp>AYERS</scp>
- Secondary instability of crossflow vortices
- Secondary instability of crossflow vortices and swept-wing boundary-layer transition
- Crossflow instability in a hypersonic boundary layer
- Global Linear Instability
This page was built for publication: Secondary instability analysis of crossflow on a hypersonic yawed straight circular cone
