Work

Shockwave/Boundary-Layer Interaction Control on a Compression Ramp Using Steady Micro Jets

Year: 2012

Type: article

Source: AIAA Journal

DOI: 10.2514/1.j051577

Authors: S. B. Verma, C. Manisankar

Institution: National Aerospace Laboratories

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: Aeronautics Research and Development Board

OpenAlex ID: W2090132718

FWCI: 3.169

Cites: 38

Cited by: 69

Related to: 10