Work

High Reynolds Number Assessment of Boundary Layer Transition Trip Drag at Mach 2.48 on HSCT Configuration

Year: 1999

Type: article

Source: NASA Technical Reports Server (NASA)

Authors: Richard A. Wahls, Melissa B. Rivers, Todd Magee, Michael Novean

Institutions: Langley Research Center, Boeing (United States)

Language: English

Topic: Fluid Dynamics and Turbulent Flows

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W826475882

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