Work

The shock tube as a device for testing transonic airfoils at high Reynolds numbers

Year: 1978

Type: conference-paper

Source: AIAA Aerodynamic Measurement Technology and Ground Testing Conference

DOI: 10.2514/6.1978-769

Authors: W. COOK, L. PRESLEY, G. CHAPMAN

Institutions: Iowa State University, Ames Research Center

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: National Aeronautics and Space Administration, Iowa State University

OpenAlex ID: W2997344680

FWCI:

Cites: 7

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Related to: 10