This report presents and discusses the results of an investigation to develop a rationale and technique for the validation of turbine engine steady-state mathematical models for use in predicting flight test performance, stability, and durability parameters. A validation procedure is derived and demonstrated using the YJ101 prototype engine AEDC test results and status deck as an example application of the technique. Typical status deck uncertainties as a function of flight condition, engine power setting, and deck input parameters are given. Status deck flight test input error effects are also given.
Turbine engine mathematical model validation
Bewertung von Turbomotoren aufgrund mathematischer Modelle
US Government Reports ; 1-43
1976
43 Seiten
Report
English