Asset Details
Do you wish to reserve the book?
Combustion Surface Calculation Method of Solid Rocket Propellant Based on Parameterized Volume Boolean Operation
Hey, we have placed the reservation for you!
By the way, why not check out events that you can attend while you pick your title.
Oops! Something went wrong.
Looks like we were not able to place the reservation. Kindly try again later.
Are you sure you want to remove the book from the shelf?
Combustion Surface Calculation Method of Solid Rocket Propellant Based on Parameterized Volume Boolean Operation
Do you wish to request the book?
Combustion Surface Calculation Method of Solid Rocket Propellant Based on Parameterized Volume Boolean Operation
Please be aware that the book you have requested cannot be checked out. If you would like to checkout this book, you can reserve another copy
We have requested the book for you!
Your request is successful and it will be processed during the Library working hours. Please check the status of your request in My Requests.
Oops! Something went wrong.
Looks like we were not able to place your request. Kindly try again later.
Journal Article
Combustion Surface Calculation Method of Solid Rocket Propellant Based on Parameterized Volume Boolean Operation
2023
Overview
In order to solve the problem of long time consuming and low efficiency in solving the complex combustion surface of solid rocket propellant, a combustion surface calculation method based on parameterized volume Boolean operation was proposed. After the solid model of propellant was created by using 3D modeling software, the parameterized burning surface model was used to perform Boolean difference calculation between the obtained burning surface growth entity and the propellant entity. Through Sensitivity Analysis function, the variation range of parameterized value was set, so as to obtain the burning face value under different burning thickness. In this paper, star shaped charge column is selected to calculate the combustion surface, and the feasibility of the method is verified. This method provides a basis for subsequent combustion surface calculation.
Publisher
IOP Publishing
