Boundary layer transition: Predictions based on linear theory
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- Type
- article
- Published
- 1994-04-01
- Cited by
- 204
- References
- 0
- OpenAlex
- https://openalex.org/W3005100859
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:118648213
Keywords
Boundary layer, Layer (electronics), Mathematics, Geometry, Statistical physics
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- A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone
- Supersonic laminar flow control techniques investigated within the SUPERTRAC project
- Supersonic laminar flow control studies in the SUPERTRAC project
- Hypersonic Boundary/Shear Layer Transition for Blunt to Slender Configurations - A NASA Langley Experimental Perspective
- Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
- Derivation of and Simulations with BiGlobal Stability Equations
- Mise en oeuvre et évaluation d’un modèle de transition à équations de transport pour la simulation d’écoulements en turbomachines
- Natural laminar flow wing for supersonic conditions: Wind tunnel experiments, flight test and stability computations
- Analysis and design of quiet hypersonic wind tunnels
- Computations for laminar flow control in swept-wing boundary layers.
- Compressible parabolized stability equation in curvilinear coordinate system and integration
- An adaptive high order Reynolds-averaged Navier-Stokes solver with transition prediction
- Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1
- Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels
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