Work

Control of shock-wave boundary layer interaction using steady micro-jets

Year: 2014

Type: article

Source: Shock Waves

DOI: 10.1007/s00193-014-0508-5

Authors: S. B. Verma, C. Manisankar, P. Akshara

Institutions: National Aerospace Laboratories, Council of Scientific and Industrial Research

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2079550668

FWCI: 1.208

Cites: 35

Cited by: 38

Related to: 10