Work

Numerical study of micro-ramp vortex generator for supersonic ramp flow control at Mach 2.5

Year: 2016

Type: article

Source: Shock Waves

DOI: 10.1007/s00193-016-0633-4

Authors: Y. Yan, L. Chen, Q. Li, C. Liu

Institutions: Huston–Tillotson University, China Academy of Launch Vehicle Technology, State Key Laboratory of Aerodynamics, The University of Texas at Arlington

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: Air Force Office of Scientific Research

Award: G1024432666

OpenAlex ID: W2302809909

FWCI: 1.439

Cites: 66

Cited by: 37

Related to: 10