Add to ORKGA number of computer codes are available for performing thermal analysis of solid rocket motor nozzl...
An annular jet flow of liquid surrounding a flow of gas at its core is extremely unstable. Axisymmet...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
The limit of large activation energy is studied for the process of simultaneous mixing and chemical ...
The paper presents a numerical method to simulate two-phase turbulent cavitating flows in ducts of v...
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
This report describes the results of a small study program in support of the design studies for NASA...
Proper acoustic excitation of a single large-eddy break-up device can increase the resulting drag re...
IBM 7094 Fortran II program for calculating turbulent boundary layer properties, with hydrogen chemi...
Carbon rug rings used to eliminate metal-metal rub of inducer on housings in rocket engine oxidizer ...
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
Interacting two-phase flow in four differently sized pneumatic two-fluid atomizers was investigated ...
Covered space, Riemann geometry extension, and partition function research on stochastic models for ...
A number of computer codes are available for performing thermal analysis of solid rocket motor nozzl...
An annular jet flow of liquid surrounding a flow of gas at its core is extremely unstable. Axisymmet...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...
Numerical analysis of internal supersonic flows with diffusion, dissipation, and hydrogen-air combus...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
The limit of large activation energy is studied for the process of simultaneous mixing and chemical ...
The paper presents a numerical method to simulate two-phase turbulent cavitating flows in ducts of v...
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
This report describes the results of a small study program in support of the design studies for NASA...
Proper acoustic excitation of a single large-eddy break-up device can increase the resulting drag re...
IBM 7094 Fortran II program for calculating turbulent boundary layer properties, with hydrogen chemi...
Carbon rug rings used to eliminate metal-metal rub of inducer on housings in rocket engine oxidizer ...
Documented is an aeronautical geometry conversion package which translates wave-drag geometry into t...
Interacting two-phase flow in four differently sized pneumatic two-fluid atomizers was investigated ...
Covered space, Riemann geometry extension, and partition function research on stochastic models for ...
A number of computer codes are available for performing thermal analysis of solid rocket motor nozzl...
An annular jet flow of liquid surrounding a flow of gas at its core is extremely unstable. Axisymmet...
Motion equations and basic control theory applied to stability and response analyses of flexible lau...