Published August 2018
| Version v1
Journal article
Improving the Lift Properties of a Wing in Takeoff and Landing by Means of a Boundary Layer Control System Using Ejector-Type Actuators
- 1. Central Aerodynamic Institute (Russian Federation)
Description
A device making it possible to control of the flow past a wing at low flight speeds is proposed. The device comprises an ejector-type actuator that simultaneous sucks the boundary layer on the upper surface and blows a gas jet in the vicinity of the trailing edge. Based on the Reynolds-averaged Navier–Stokes equations, a mathematical model of an ejector-type actuator is developed and experimental studies are carried out.
Additional details
Identifiers
Publishing Information
- Journal Title
- Technical Physics Letters
- Journal Volume
- 44
- Journal Issue
- 8
- Journal Page Range
- p. 687-690
- ISSN
- 1063-7850
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 50029581
- Subject category
- S75: CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY;
- Descriptors DEI
- BOUNDARY LAYERS; COMPUTERIZED SIMULATION; CONTROL SYSTEMS; EQUATIONS; NAVIER-STOKES EQUATIONS; REYNOLDS NUMBER; SURFACES
- Descriptors DEC
- DIFFERENTIAL EQUATIONS; DIMENSIONLESS NUMBERS; EQUATIONS; LAYERS; PARTIAL DIFFERENTIAL EQUATIONS; SIMULATION
Optional Information
- Copyright
- Copyright (c) 2018 Pleiades Publishing, Ltd.