Recently, a turbine-brush was analyzed based on the energy conservation and the force momentum equation with an empirical relationship of the drag coefficient. An equation was derived to predict the rotational speed of the turbine-brush in terms of the blade angle, number of blades, rest of geometries of the turbine-brush and the incoming velocity. Using the observed flow conditions, drag coefficients were determined. Based on the experimental values as boundary conditions, the turbine-brush flows were numerically simulated to understand first the nature of the flows, and to extend the observed drag coefficient to a flow without holding the turbine-brush
An analytical computational concept is presented which predicts the temperature profiles along a reg...
Frequencies below 10 GHz continue to be used for a large portion of satellite service, and new appli...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The Calibrated Ancillary System (CAS) provides real-time calibrated parameters from the orbiter down...
Design procedures for a new low-speed boundary-layer research channel are described. The channel is ...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
NASA-Redox systems are electrochemical storage devices that use two fully soluble Redox couples, ano...
Numerical methods have been developed for obtaining the steady, adiabatic flow field of a frictionle...
The automatic landing of an unpowered space shuttle vehicle was studied along with the design of the...
The goal of this project is to supplement the footwear design system of North Carolina State Univers...
A 203rd order simulation model was developed to evaluate the space station customer accommodation pa...
The results are reported of a program to develop special instrumentation systems and engine hardware...
The present invention is directed to a method and apparatus for interactively analyzing the characte...
NASA's Space Station Freedom proposed hybrid power system includes photovoltaic arrays with nickel h...
Relationship between dynamic contact angle and velocity of liquid front along solid surfac
An analytical computational concept is presented which predicts the temperature profiles along a reg...
Frequencies below 10 GHz continue to be used for a large portion of satellite service, and new appli...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The Calibrated Ancillary System (CAS) provides real-time calibrated parameters from the orbiter down...
Design procedures for a new low-speed boundary-layer research channel are described. The channel is ...
Volume two of the facilities catalogue deals with Airbreathing Propulsion and Flight Simulation Faci...
NASA-Redox systems are electrochemical storage devices that use two fully soluble Redox couples, ano...
Numerical methods have been developed for obtaining the steady, adiabatic flow field of a frictionle...
The automatic landing of an unpowered space shuttle vehicle was studied along with the design of the...
The goal of this project is to supplement the footwear design system of North Carolina State Univers...
A 203rd order simulation model was developed to evaluate the space station customer accommodation pa...
The results are reported of a program to develop special instrumentation systems and engine hardware...
The present invention is directed to a method and apparatus for interactively analyzing the characte...
NASA's Space Station Freedom proposed hybrid power system includes photovoltaic arrays with nickel h...
Relationship between dynamic contact angle and velocity of liquid front along solid surfac
An analytical computational concept is presented which predicts the temperature profiles along a reg...
Frequencies below 10 GHz continue to be used for a large portion of satellite service, and new appli...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...