Modular Method for Estimation of Velocity and Temperature Profiles in High-Speed Boundary Layers-Reference-Cited by-同舟云学术

Modular Method for Estimation of Velocity and Temperature Profiles in High-Speed Boundary Layers

Published:2022-09 Issue:9 Volume:60 Page:5165-5172
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kumar Vedant¹^ORCID,Larsson Johan¹^ORCID

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Funder

Air Force Office of Scientific Research Hypersonics program

NASA Transformational Tools and Technologies project

Innovative and Novel Computational Impact on Theory and Experiment (INCITE) program at the Argonne Leadership Computing Facility

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061735

Reference34 articles.

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2. Low-Reynolds-Number Turbulent Boundary Layers in Zero and Favorable Pressure Gradients

3. Approach to an asymptotic state for zero pressure gradient turbulent boundary layers

4. SommerS. C.ShortB. J. “Free-Flight Measurements of Turbulent-Boundary-Layer Skin Friction in the Presence of Severe Aerodynamic Heating at Mach Numbers from 2.8 to 7.0,” NACA TN 3391, 1955.

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