Withdrawal: Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel
Year: 2019
Type: conference-paper
Source: AIAA SciTech Forum
Institution: Langley Research Center
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W3180960591
