Reference health
Direct numerical simulation of breakdown to turbulence in a Mach 6 boundary layer over a porous surface
39/39 checkable references clean · checked 2026-07-25
Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.
7 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.
The 39 checked references that resolve
resolves10.2514/3.49694
Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition
resolves10.1063/1.857897
Effect of heat transfer on the subharmonic instability of compressible boundary layers
resolves10.1017/S0022112094001965
Oblique-mode breakdown and secondary instability in supersonic boundary layers
resolves10.1007/BF00849118
Direct simulation of breakdown to turbulence following oblique instability waves in a supersonic boundary layer
resolves10.1017/S0022112096000766
Subharmonic transition to turbulence in a flat-plate boundary layer at Mach number 4.5
resolves10.1007/s001620050080
Direct Numerical Simulation of Hypersonic Boundary-Layer Flow on a Flared Cone
resolves10.1017/S0022112008003030
Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone
resolves10.1017/S0022112000002147
Leading-edge receptivity of a hypersonic boundary layer on a flat plate
resolves10.1017/S0022112003005263
Receptivity of a high-speed boundary layer to acoustic disturbances
resolves10.1063/1.2013261
Initial-value problem for three-dimensional disturbances in a compressible boundary layer
resolves10.1017/S0022112003004786
Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
resolves10.1017/S0022112003004798
Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound
resolves10.1017/S0022112007007070
Response of a compressible laminar boundary layer to free-stream vortical disturbances
resolves10.2514/2.1671
Experiments on Passive Hypervelocity Boundary-Layer Control Using an Ultrasonically Absorptive Surface
resolves10.1017/S0022112002003440
Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating
resolves10.2514/6.2007-948
Direct Numerical Simulation of Supersonic Boundary-Layer Stabilization by Porous Coatings
resolves10.2514/6.2008-3903
Interaction of Acoustic Disturbances with Micro-Cavities for Ultrasonic Absorptive Coatings
resolves10.2514/1.43388
Numerical Study of Mach 6 Boundary-Layer Stabilization by Means of a Porous Surface
resolves10.2514/6.2009-7202
Stability Analysis of Hypersonic Boundary Layer Flow over Microporous Surfaces
resolves10.1146/annurev.fl.23.010191.002431
Numerical Simulation of Transition in Wall-Bounded Shear Flows
resolves10.1006/jcph.1998.6114
A Stable and Conservative Interface Treatment of Arbitrary Spatial Accuracy
resolves10.1006/jcph.2002.7022
Entropy Splitting for High-Order Numerical Simulation of Compressible Turbulence
resolves10.1063/1.858291
Secondary instability of high-speed flows and the influence of wall cooling and suction
resolves10.2514/6.2010-1242
Temporal Stability of Hypersonic Boundary Layer on Porous Wall: Comparison of Theory with DNS
The 7 references without a DOI — listed, not checked
no DOI — not checkedL. Lees and C. C. Lin, “Investigation of the stability of the laminar boundary layer in a compressible fluid,” NACA Technical Report No. 1115, 1946.
no DOI — not checkedL. M. Mack, “Boundary layer linear stability theory,” AGARD Technical Report No. 705, 1984.
no DOI — not checkedL. Lees, “The stability of the laminar boundary layer in a compressible fluid,” NACA Technical Report No. 1360, 1947.
no DOI — not checkedA. A. Maslov, “Experimental and theoretical studies of hypersonic laminar flow control using ultrasonically absorptive coatings (UAC),” ITSC Technical Report No. 2172-2001, 2003.
no DOI — not checkedA. A. Wray, “Minimal storage time advancement schemes for spectral methods,” NASA Ames Research Center Report No. M.S. 202 A-1, 1990.
no DOI — not checkedJ. T. Stuart, “The production of intense shear layers by vortex stretching and convection,” AGARD Technical Report No. 514, 1965.
no DOI — not checkedFundamentals of Ocean Acoustics
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work were clean at the dated check: each resolved to a known work in a public registry, and none
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