Ir directamente a la navegación principal Ir directamente a la búsqueda Ir directamente al contenido principal

Experimental and numerical study of Carbon Fiber Oxidation

Producción científica: Paperrevisión exhaustiva

6 Citas (Scopus)

Resumen

The oxidation at high Knudsen number of FiberForm ®, the matrix material of NASA's Phenolic Impregnated Carbon Ablator, is investigated both experimentally and numerically. The experimental setup consists of a quartz tube through a clamshell heater. Mass loss and recession of carbon preform samples are measured at temperatures between 700 and 1300 K and pressures around 2000 Pa. A volume average fiber-scale oxidation model is used to model the setup and extract the effective reactivity of the material. New values for carbon fiber reactivity are suggested and discussed.

Idioma originalEnglish
EstadoPublished - 2014
Evento52nd Aerospace Sciences Meeting 2014 - National Harbor, United States
Duración: ene 13 2014ene 17 2014

Conference

Conference52nd Aerospace Sciences Meeting 2014
País/TerritorioUnited States
CiudadNational Harbor
Período1/13/141/17/14

Nota bibliográfica

Publisher Copyright:
© 2014, American Institute of Aeronautics and Astronautics Inc. All rights reserved.

ASJC Scopus subject areas

  • Aerospace Engineering

Huella

Profundice en los temas de investigación de 'Experimental and numerical study of Carbon Fiber Oxidation'. En conjunto forman una huella única.

Citar esto