La Recherche Aerospatiale, Bimonthly Bulletin, no. 1982-6, 211/November-Decemter 1982
Abstract
A modular method for centrifugal compressor performance prediction is presented. Cyclic hardening of stainless steel under complex loading is described. Fatigue failure microinitiation, micropropagation and damage is considered. The stability of a tilting rotor aircraft model is studied. The thermal stability of titanium alloys is investigated. A compensator for thermal effects on quartz oscillators is described.
- Publication:
-
La Recherche Aerospatiale
- Pub Date:
- April 1983
- Bibcode:
- 1983ReAeB....S....S
- Keywords:
-
- Centrifugal Compressors;
- Hardening (Materials);
- Microcracks;
- Tilt Rotor Aircraft;
- Titanium Alloys;
- Voltage Controlled Oscillators;
- Aerodynamic Stability;
- Crystal Oscillators;
- Prediction Analysis Techniques;
- Quartz Crystals;
- Thermal Fatigue;
- Thermal Stability;
- Transonic Flutter;
- Engineering (General)