Related Concept Videos
Time-Domain Interpretation of PD Control
Consider the example of control of motor torque. Initially, a positive...
Turbine-Governor Control
Turbulent Flow
PD Controller: Design
Designing a continuous-data controller requires selecting and linking components like adders and integrators, which are fundamental in Proportional,...
Steady, Laminar Flow Between Parallel Plates
Multi-input and Multi-variable systems
In the absence of...
You might also read
Related Articles
Articles linked to this work by shared authors, journal, and citation graph.
Automated Local Measurement of Wall Shear Stress with AI-Assisted Oil Film Interferometry.
Revival of classical vortex generators now for transition delay.
Related Experiment Video
Updated: Apr 27, 2026

A Rapid Method for Modeling a Variable Cycle Engine
Published on: August 13, 2019
Consecutive turbulence transition delay with reinforced passive control.
Sohrab S Sattarzadeh1, Jens H M Fransson1, Alessandro Talamelli2
1Linné Flow Centre, KTH Royal Institue of Technology, SE-10044 Stockholm, Sweden.
Using a second array of miniature vortex generators (MVGs) prolongs laminar flow control, delaying turbulence transition and achieving over 65% skin-friction drag reduction.
Area of Science:
- Fluid dynamics
- Aerodynamics
- Boundary layer theory
Background:
- Miniature vortex generators (MVGs) can delay turbulence transition in flat plate boundary layers.
- The laminar control effect of single-array MVGs diminishes rapidly due to exponential flow recovery.
Purpose of the Study:
- To investigate the efficacy of a dual-array MVG system for sustained laminar flow control.
- To enhance the streamwise extent and effectiveness of laminar flow control.
- To achieve significant skin-friction drag reduction.
Main Methods:
- Implementation of a second array of MVGs downstream of an initial array.
- Analysis of the interaction and reinforcement of counter-rotating streamwise vortices.
- Experimental or computational fluid dynamics (CFD) investigation of the modulated boundary layer flow.
Main Results:
- The second MVG array successfully nourishes the streamwise vortices, extending the laminar control.
- The dual-array system significantly prolongs the streamwise region of laminar flow.
- A net skin-friction drag reduction exceeding 65% was demonstrated.
Conclusions:
- A dual-array MVG strategy offers a viable method for prolonged laminar flow control.
- This approach effectively overcomes the rapid decay of passive laminar control.
- Significant aerodynamic drag reduction is achievable through this enhanced vortex generation technique.
