Flow Visualization of Four-Inlet Ducted Rocket Engine Configurations
Title | Flow Visualization of Four-Inlet Ducted Rocket Engine Configurations PDF eBook |
Author | |
Publisher | |
Pages | 0 |
Release | 1990 |
Genre | |
ISBN |
A water flow visualization facility was constructed in order to investigate the mixing processes inside of four-inlet ducted rocket engines (DRE) with various flow rates and geometries. The observed flow fields were documented with video and conventional photography so that relationships between various geometric/flow parameters and the flow field behavior could be obtained.
Characterization of Four-inlet Ducted Rocket Engine Geometries : an Optical Diagnostics Approach
Title | Characterization of Four-inlet Ducted Rocket Engine Geometries : an Optical Diagnostics Approach PDF eBook |
Author | Christopher Michael Brophy |
Publisher | |
Pages | 194 |
Release | 1997 |
Genre | Rocket engines |
ISBN |
33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Title | 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit PDF eBook |
Author | |
Publisher | |
Pages | 562 |
Release | 1997 |
Genre | Airplanes |
ISBN |
Modelling and Flow Visualization of Mixing in a Ducted Rocket Combustor
Title | Modelling and Flow Visualization of Mixing in a Ducted Rocket Combustor PDF eBook |
Author | R. A. Stowe |
Publisher | |
Pages | |
Release | 1998 |
Genre | |
ISBN |
32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Title | 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit PDF eBook |
Author | |
Publisher | |
Pages | 420 |
Release | 1996 |
Genre | Airplanes |
ISBN |
An Investigation of Four-inlet Ducted Rocket Engine Flame-holding Characteristics
Title | An Investigation of Four-inlet Ducted Rocket Engine Flame-holding Characteristics PDF eBook |
Author | Christopher M. Brophy |
Publisher | |
Pages | |
Release | 1997 |
Genre | |
ISBN |
Static Thrust Augmentation of a Rocket-ejector System with a Heated Supersonic Primary Jet
Title | Static Thrust Augmentation of a Rocket-ejector System with a Heated Supersonic Primary Jet PDF eBook |
Author | Albert J. Simonson |
Publisher | |
Pages | 32 |
Release | 1962 |
Genre | Aerodynamics, Supersonic |
ISBN |
"An investigation was conducted in order to evaluate the static thrust augmentation attainable through the use of a rocket-ejector system with a heated supersonic primary jet. This system consisted of a cylindrical mixing tube in conjunction with a supersonic nozzle having an expansion ratio of 15 to 1. A hydrogen peroxide gas generator was used to provide heated nozzle flow. An ejector with a bellmouthed inlet provided thrust augmentation up to about 18 percent of the primary rocket thrust, whereas the use of a blunt-lip inlet with elliptical profile provided augmentation up to 9 percent. Axial withdrawal of the rocket nozzle from the ejector provided small gains in thrust augmentation."--P.[1]