Reference health

On the influence of trailing-edge serrations on open-rotor tonal noise

https://doi.org/10.2514/6.2012-2124
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14/14 checkable references clean · checked 2026-08-20

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.

8 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 14 checked references that resolve
resolves10.2514/6.1986-1474
Turbofan and propfan as basis for future economic propulsion concepts
resolves10.2514/6.1988-2807
UHB technology validation - The final step
resolves10.2514/6.2010-3710
Ffowcs Williams & Hawkings Formulation for the Convective Wave Equation and Permeable Data Surface
resolves10.2514/6.2011-2759
Similarities of the free-field and in-duct formulations in rotor noise problems
resolves10.2514/6.2012-2127
Aerodynamic and Basic Acoustic Optimization of a Counter Rotating Open Rotor with Experimental Verification
resolves10.2514/6.2012-2303
Open-rotor noise prediction with a RANS-informed analytical method
resolves10.1016/0021-9991(81)90128-5
Approximate Riemann solvers, parameter vectors, and difference schemes
resolves10.2514/3.10521
Nonreflecting boundary conditions for Euler equation calculations
resolves10.1115/1.2162182
Toward Excellence in Turbomachinery Computational Fluid Dynamics: A Hybrid Structured-Unstructured Reynolds-Averaged Navier-Stokes Solver
resolves10.1006/jsvi.1996.0843
A NEW BOUNDARY INTEGRAL FORMULATION FOR THE PREDICTION OF SOUND RADIATION
resolves10.2514/2.558
Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces
resolves10.1260/147547203322775498
Surface Integral Methods in Computational Aeroacoustics—From the (CFD) Near-Field to the (Acoustic) Far-Field
resolves10.1260/1475472054771376
Noise Prediction for Increasingly Complex Jets. Part I: Methods and Tests
resolves10.1260/147547209788549280
Variants of the Ffowcs Williams - Hawkings Equation and Their Coupling with Simulations of Hot Jets
The 8 references without a DOI — listed, not checked
no DOI — not checkedProceedings of ASME Turbo Expo, 2010, GT2010-22076
no DOI — not checked14th CEAS-ASC Workshop & 5th Scientific Workshop of X3-Noise, Aeroacoustics of high-speed aircraft propellers and open rotors
no DOI — not checkedProceedings of the 15th International Symposium on Air Breathing Engines
no DOI — not checkedDGLR-JT2002-073
no DOI — not checkedProceedings of the ASME Turbo-Expo, Wien, Österreich, 7.-14
no DOI — not checkedDLR Köln
no DOI — not checkedProceedings of ASME Turbo Expo, 2009, GT2009-59332
no DOI — not checkedDiplomarbeit
What this badge says. CiteStamped means the CHECKABLE references of this work were clean at the dated check: each resolved to a known work in a public registry, and none carried a retraction notice at that time. It says nothing about the quality, findings, or importance of the work itself, and nothing about references deposited without a DOI.

checked 2026-08-20 — re-checked daily as this page is visited; titles and statuses come from Crossref and DataCite and are not part of the signed record

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