Record Nr.

UNINA9910704816803321

Autore

Csank Jeffrey T.

Titolo

Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber

Pubbl/distr/stampa


Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013]

Descrizione fisica

1 online resource (12 pages) : illustrations

Collana

NASA/TM ; ; 2013-216515

Soggetti

Inlet flow

Controllers

Feedback control

Computerized simulation

Turbine engines

Engine inlets

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

Title from title screen (viewed Nov. 13, 2013).

"May 2013."

Nota di bibliografia

Includes bibliographical references (pages 11-12).