scholarly journals Multiphysics Computational Analysis of a Solid-Core Nuclear Thermal Engine Thrust Chamber

2007 ◽  
Author(s):  
Ten-See Wang ◽  
Francisco Canabal ◽  
Yen-Sen Chen ◽  
Gary Cheng
Keyword(s):  
Computational Analysis ◽  
Solid Core ◽  
Thrust Chamber ◽  
Engine Thrust

scholarly journals Multiphysics Computational Analysis of a Solid-Core Nuclear Thermal Engine Thrust Chamber

2010 ◽  
Vol 26 (3) ◽  
pp. 407-414 ◽  
Author(s):  
Ten-See Wang ◽  
Francisco Canabal ◽  
Yen-Sen Chen ◽  
Gary Cheng
Keyword(s):  
Computational Analysis ◽  
Solid Core ◽  
Thrust Chamber ◽  
Engine Thrust

Thermostructural Analysis of Rocket Engine Thrust Chamber

2015 ◽  
Vol V4 (08) ◽  
Author(s):  
Santhini S Lal ◽  
A. K. Asraff ◽  
Shobha Elizebath Thomas ◽  
Keyword(s):  
Rocket Engine ◽  
Thrust Chamber ◽  
Engine Thrust

Computational Analysis of Blended Winglet Model Performance by Varying Cant Angle

2019 ◽  
Vol 16 (2) ◽  
pp. 467-471
Author(s):  
Bino Prince D. Raja ◽  
G. Ramanan ◽  
Diju G. Samuel
Keyword(s):  
Fuel Consumption ◽  
Computational Analysis ◽  
Model Performance ◽  
Aircraft Engine ◽  
Modeling And Analysis ◽  
Engine Thrust ◽  
Ansys Cfx ◽  
Inclination Angles ◽  
Important Challenge ◽  
Control Surfaces

This work focuses on structural modeling and analysis of aircraft winglet control surfaces. In aerodynamic engineering, reducing drag is an important challenge. To reduce drag a fin device that is placed vertically in the angle set in the wing of the plane. Winglet design reduces fuel consumption by reducing the drag of the aircraft and will make the aircraft more stable during the flight, will also give the aircraft engine more time to reduce the load on the engine thrust life. The goal is to design and simulate a winglet aircraft model using software such as CATIA V5-which is used to build fin models and ANSYS CFX solver is used to test and simulate model fins. With winglets without fins it analyzes change the inclination angles, the results are compared and plotted. Fins are an important part of an aircraft that reduces the amount of drag and fuel consumption by using less energy while reducing wing vortexes.

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