Acoustics and Thrust of Separate-Flow Exhaust Nozzles With Mixing Devices for High-Bypass-Ratio Engines

doi 10.2514/6.2000-1961
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Numerical Studies on Thrust Augmentation in High Area Ratio Rocket Nozzles by Secondary Injection

Journal of Applied Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2017English

Flashboiling Atomization in Nozzles for GDI Engines

2017English

Optimum Mixing of Core- And Bypass-Streams in a High Bypass Civil Turbofan

2001English

External Losses in High-Bypass Turbo Fan Air Engines

International Journal of Exergy
Energy
2008English

Flow Separation in Rocket Nozzles Under High Altitude Condition

Shock Waves
AstronomyPhysicsMechanical Engineering
2016English

Increase of Durability of Injector Nozzles Automotive Diesel Engines

Agricultural Bulletin of Stavropol Region
2018English

Pressure Distribution and Performance Impacts of Aerospike Nozzles on Rotating Detonation Engines

2018English

Exhaust Characteristics of LPG/Gas-Oil Diesel Engines.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
1998English

A Study on Diesel Combustion With High-Pressure Fuel Injection. Improvement of Combustion and Exhaust Emissions Using Small-Hole-Diameter Nozzles.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
1994English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy