VFS Website
  • VIEW CART
  • CUSTOMER SUPPORT
  • MY STORE ACCOUNT
  • CONTACT US
  • STORE HOME
  • 5Prime
  • Forum Proceedings
  • Workshops
  • Technical Meetings
  • Vertiflite
  • Books, CDs & Gifts


Unable to log in or get member pricing? Having trouble changing your password?

Please review our Frequently Asked Questions for complete information on these and other common situations.
 

Vertical Flight Library & Store

CHECKOUT

0 Item(s) In Cart Total: $0.00


High Temperature Ceramic Matrix Composite Materials Research for Next Generation Army Propulsion System

Anindya Ghoshal, Muthuvel Murugan, Andy Nieto, Michael Walock, Luis Bravo, Marc Pepi, Jeffrey Swab, U.S. Army Research Laboratory; Clara Hofmeister Mock, Oak Ridge Institute for Science, Education; Samuel Hirsch, Robert Dowding, U.S. Army Research Laboratory

  • Your Path :
  • Home
  • > High Temperature Ceramic Matrix Composite Materials Research for Next Generation Army Propulsion System

High Temperature Ceramic Matrix Composite Materials Research for Next Generation Army Propulsion System

  • Presented at Forum 74
  • 16 pages
  • SKU # : 74-2018-1356
  • Your Price : $30.00
  • Join or log in to receive the member price of $15.00!


VFS member?
Don't add this to your cart just yet!
Be sure to log in first to receive the member price of $15.00!

 
Add To Cart

Add to Wish List

Reward Value:
(60) Member Points

High Temperature Ceramic Matrix Composite Materials Research for Next Generation Army Propulsion System

Authors / Details: Anindya Ghoshal, Muthuvel Murugan, Andy Nieto, Michael Walock, Luis Bravo, Marc Pepi, Jeffrey Swab, U.S. Army Research Laboratory; Clara Hofmeister Mock, Oak Ridge Institute for Science and Education; Samuel Hirsch, Robert Dowding, U.S. Army Research Laboratory

Abstract
Aviation propulsion system structures are subjected to challenging conditions such as extremely high velocities, ultra- high/low temperatures, and excessive dust/sand/smoke/volcanic ash conditions during military operations. Therefore, the research and development of high-performance engine materials with superior characteristics such as great mechanical strength, high fatigue resistance and creep resistance, good tolerance to wide temperature variations, and excellent resistance to corrosion and oxidation is essential to the evolution of highly robust and efficient propulsion systems without a compromise on capabilities, even in hostile environments. The goal of this collaborative program within United States Army Research Laboratory (ARL) is to establish a generalized fundamental physics-based approach and probabilistic-based lifing method to extrapolate thermal loading performance and material characterization results from high performance high temperature ceramic materials such as ceramic matrix composites (CMC) based flat specimens and engine component representative specimens. High temperature structural integrity and durability and probabilistic-based lifing assessment will be evaluated both analytically and experimentally under thermal shock, thermal cycling, and combined thermo-mechanical loadings. This paper presents the ARL CMC propulsion materials strategy in each of the identified thrust areas and present some results from some of the ongoing research at ARL and its research partners.

Recently Viewed Items

  • High Temperature Ceramic Matrix Composite Materials Research for Next Generation Army Propulsion System

    Member Price :
    $15.00
    Your Price :
    $30.00

Popular Products

  • Master Card
  • Visa
  • American Express
  • Customer Support
  • Contact Us
  • Privacy and Security Policies
  • Refund Policies

Copyright © 2022 The Vertical Flight Society. All rights reserved.