A parametric cycle analysis and a preliminary recuperator design study were conducted for a 500-hp intermediate rated power (IRP) recuperative helicopter engine. The U-tube recuperator with airflow inside the tubes and single cross flow gas path was found to be the lightest design in the 0.6-0.8 effectiveness range considered for the cycle analysis. (Stoehr)
Regenerative engine analysis program
Analyse eines rekuperativen Hubschrauberantriebs
US Government Reports ; Jan ; 1-199
1981
199 Seiten
Report
Englisch
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