A multiyear project to assemble a robust, muitiphase spray combustion code is now underway and gradually building up to full speed. The overall effort involves several university and government research teams as well as Rocketdyne. The first part of this paper will give an overview of the respective roles of the different participants involved, the master strategy, the evolutionary milestones, and an assessment of the state-of-the-art of various key components. The second half of this paper will highlight the progress made to date in extending the baseline Navier-Stokes solver to handle multiphase, multispecies, chemically reactive sub- to supersonic flows. The major hurdles to overcome in order to achieve significant speed ups are delineat...
Acousto-ultrasonics utilizes simulated stress waves to detect and quantify defect states, damage con...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
The requirements for space shuttle emergency intravehicular activity support equipment are discussed...
A very important consideration in turbopump design is the prediction and prevention of cavitation. T...
In order to meet the anticipated needs in modeling and analysis of advanced aerospace structures, NA...
The design of turbomachinery blades requires the prevention of flutter for all operating conditions....
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
Many sophisticated mathematical control techniques for flexible structures have been devised. The ba...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
Research is in progress to develop flight strategy concepts for avoidance and recovery from microbur...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
Development and assessment of the single-time-scale k-epsilon turbulence model with different near-w...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
Vugraphs are presented on the effect of cruise Mach number on the maximum takeoff weight of the High...
Acousto-ultrasonics utilizes simulated stress waves to detect and quantify defect states, damage con...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
The requirements for space shuttle emergency intravehicular activity support equipment are discussed...
A very important consideration in turbopump design is the prediction and prevention of cavitation. T...
In order to meet the anticipated needs in modeling and analysis of advanced aerospace structures, NA...
The design of turbomachinery blades requires the prevention of flutter for all operating conditions....
An outline of the organization and capabilities of the Engine Structures Computational Simulator (Si...
The Control of Flexible Structures II (CPFS) program is a complex and ambitious undertaking which ad...
Many sophisticated mathematical control techniques for flexible structures have been devised. The ba...
The following pages describe the development of a nonlinear simulation, results for the Martian entr...
Research is in progress to develop flight strategy concepts for avoidance and recovery from microbur...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
Development and assessment of the single-time-scale k-epsilon turbulence model with different near-w...
A point mass, three-degree of freedom model is presented as a basic development tool for PC based si...
Vugraphs are presented on the effect of cruise Mach number on the maximum takeoff weight of the High...
Acousto-ultrasonics utilizes simulated stress waves to detect and quantify defect states, damage con...
Film/dump cooling a rocket nozzle with fuel rich gas, as in the National Launch System (NLS) Space T...
The requirements for space shuttle emergency intravehicular activity support equipment are discussed...