Computation of Trailing-Edge Noise Due to Turbulent Flow over an Airfoil
Year: 2002
Type: article
Source: AIAA Journal
DOI: 10.2514/2.1582
Institution: Stanford University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Office of Naval Research
OpenAlex ID: W2046653745
