Skip to content
DraconiticResearch
Search Sources API
186,541 studies31 sourcesUpdated 5 min ago
PreprintarXiv licencearXiv

Mapping-based exact-integral formulation of skin-friction transformations for zero-pressure-gradient compressible turbulent boundary layers

Abstract

A long-standing route to efficient surface-drag prediction in zero-pressure-gradient compressible turbulent boundary layers is to map the skin-friction coefficient Cf and momentum-thickness Reynolds number Reθ onto their `incompressible' counterparts. Reassessment against an extensive DNS database shows that existing formulations do not consistently recover the reference incompressible skin-friction behaviour, even when transformed data exhibit improved collapse. We define the mapped `incompressible' state as a constant-property counterpart of the physical compressible boundary layer and derive the transformation factors from prescribed mean-velocity and wall-normal-coordinate mappings. This definition-first approach links skin-friction scaling to the full-layer accuracy of the underlying velocity transformation and exposes inherited outer-layer errors. Van Driest's theory is recast in a finite-Re exact-integral form, with the classical vD I and II transformations recovered as leading-order asymptotic reductions. Their limitations at finite Reynolds numbers are quantified, and the historical success of vD II is traced to a fortuitous cancellation of truncation errors. The exact-integral formulation then yields modified transformations assessed through a priori scaling and standalone a posteriori prediction of Cf from prescribed macroscopic and wall-thermal inputs. The VIPL-based modified transformation gives the best overall performance. Across 0.30 ≤ M∞ ≤ 13.64 and −0.55 ≤ varTheta ≤ 2.85, its prediction errors remain below 11%, with a mean error of 3.07%. Overall, the analysis places skin-friction transformations on a mapping-based exact-integral footing, relating them directly to prescribed mean-flow mappings while avoiding the leading-order asymptotic truncations that limit classical van Driest theory at finite Reynolds numbers.

Related

  1. Modelling friction and heat transfer in turbulent forced convection over porous lattices
    Aneek Chakraborty, Stefan Hickel, Davide Modesti
    arXivPreprintCC BY 4.0Full textFluid dynamicsarXiv
  2. Controlling Turbulent Flows in Compressible Active Liquid Crystals
    Dimitrios Krommydas, Paarth Gulati, Aparna Baskaran +1
    arXivPreprintCC BY 4.0Full textBiological & medical physicsCondensed matterarXiv
  3. Integral transformations for conformally invariant celestial amplitudes
    Aphiwat Yuenyong, Pongwit Srisangyingcharoen, Ekapong Hirunsirisawat +1
    Physics Letters BPeer-reviewedCC BY 4.0Full textHigh-energy & particle physicsCrossref
  4. Integral relations for the skin-friction coefficients and other quantities of annular flows
    Pierre Ricco
    arXivPreprintCC BY 4.0Full textFluid dynamicsarXiv
  5. Quantum-Inspired Computational Fluid Dynamics for Transient Turbulent Compressible Flows
    Shang Xian Matthew Lee, Melissa Kozul, Muhammad Usman +3
    arXivPreprintCC BY 4.0Full textFluid dynamicsQuantum physics & quantum informationarXiv
BibTeX
@misc{zhu2026mappingbased,
  title = {{Mapping-based exact-integral formulation of skin-friction transformations for zero-pressure-gradient compressible turbulent boundary layers}},
  author = {Xuke Zhu and Xiaoshuo Yang and Yongchao Ji and Shiyi Chen and Zhenhua Xia},
  howpublished = {arXiv},
  year = {2026},
  month = sep,
  doi = {10.48550/arxiv.2609.02650},
  eprint = {2609.02650},
  archivePrefix = {arXiv},
  url = {https://arxiv.org/abs/2609.02650},
}
RIS
TY  - UNPB
TI  - Mapping-based exact-integral formulation of skin-friction transformations for zero-pressure-gradient compressible turbulent boundary layers
AU  - Xuke Zhu
AU  - Xiaoshuo Yang
AU  - Yongchao Ji
AU  - Shiyi Chen
AU  - Zhenhua Xia
PY  - 2026
DA  - 2026/09/02
PB  - arXiv
DO  - 10.48550/arxiv.2609.02650
UR  - https://arxiv.org/abs/2609.02650
AB  - A long-standing route to efficient surface-drag prediction in zero-pressure-gradient compressible turbulent boundary layers is to map the skin-friction coefficient C_f and momentum-thickness Reynolds number Re_θ onto their `incompressible' counterparts. Reassessment against an extensive DNS database shows that existing formulations do not consistently recover the reference incompressible skin-friction behaviour, even when transformed data exhibit improved collapse. We define the mapped `incompressible' state as a constant-property counterpart of the physical compressible boundary layer and derive the transformation factors from prescribed mean-velocity and wall-normal-coordinate mappings. This definition-first approach links skin-friction scaling to the full-layer accuracy of the underlying velocity transformation and exposes inherited outer-layer errors. Van Driest's theory is recast in a finite-Re exact-integral form, with the classical vD I and II transformations recovered as leading-order asymptotic reductions. Their limitations at finite Reynolds numbers are quantified, and the historical success of vD II is traced to a fortuitous cancellation of truncation errors. The exact-integral formulation then yields modified transformations assessed through a priori scaling and standalone a posteriori prediction of C_f from prescribed macroscopic and wall-thermal inputs. The VIPL-based modified transformation gives the best overall performance. Across 0.30 ≤ M_∞ ≤ 13.64 and −0.55 ≤ varTheta ≤ 2.85, its prediction errors remain below 11%, with a mean error of 3.07%. Overall, the analysis places skin-friction transformations on a mapping-based exact-integral footing, relating them directly to prescribed mean-flow mappings while avoiding the leading-order asymptotic truncations that limit classical van Driest theory at finite Reynolds numbers.
ER  -