The next generation of subsonic commercial aircraft will require engines with improved efficiency an...
The objective of the Advanced High Temperature Engine Materials Technology Program (HITEMP) is to ge...
Advanced aircraft engine research within NASA Lewis is being focused on propulsion systems for subso...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Determining mechanical properties and air-oxidation behavior of chromium-base compositions at temper...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Significant progress has recently been made in many high temperature material categories pertinent t...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
High Temperature issues in aircraft engines Hot section: Ni and Co based Superalloys Oxidation and C...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
NASA Headquarters and LeRC have advocated an Enabling Propulsion Materials Program (EPM) to begin in...
Materials for future generations of aeropropulsion systems will be required to perform at ever-incre...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The next generation of subsonic commercial aircraft will require engines with improved efficiency an...
The objective of the Advanced High Temperature Engine Materials Technology Program (HITEMP) is to ge...
Advanced aircraft engine research within NASA Lewis is being focused on propulsion systems for subso...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Determining mechanical properties and air-oxidation behavior of chromium-base compositions at temper...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Significant progress has recently been made in many high temperature material categories pertinent t...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
High Temperature issues in aircraft engines Hot section: Ni and Co based Superalloys Oxidation and C...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
NASA Headquarters and LeRC have advocated an Enabling Propulsion Materials Program (EPM) to begin in...
Materials for future generations of aeropropulsion systems will be required to perform at ever-incre...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The next generation of subsonic commercial aircraft will require engines with improved efficiency an...
The objective of the Advanced High Temperature Engine Materials Technology Program (HITEMP) is to ge...
Advanced aircraft engine research within NASA Lewis is being focused on propulsion systems for subso...