Visualization of Pressure and Skin-Friction Fields on Rotating Blade Under Low-Pressure Conditions-Reference-Cited by-同舟云学术

Visualization of Pressure and Skin-Friction Fields on Rotating Blade Under Low-Pressure Conditions

Published:2022-09 Issue:9 Volume:60 Page:5422-5435
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Nagata Takayuki¹^ORCID,Sato Hitomi¹,Okochi Masaki¹,Matsuyama Takafumi¹,Sugioka Yosuke¹,Kasai Miku¹^ORCID,Kusama Kensuke¹,Numata Daiju¹,Nonomura Taku¹^ORCID,Asai Keisuke¹

Affiliation:

1. Tohoku University, Sendai 980-8579, Japan

Funder

Core Research for Evolutional Science and Technology

Japan Society for the Promotion of Science

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061638

Reference76 articles.

1. Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel

2. Effect of Mach Number on Airfoil Characteristics at Reynolds Number of 3,000

3. Investigation of Mach number effects on flow over a flat plate at Reynolds number of 1.0 × 104 by schlieren visualization

4. Stability of the Low Reynolds Number Compressible Flow Past a NACA0012 Airfoil

5. Compressibility effects on flat-plates with serrated leading-edges at a low Reynolds number

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