Record Nr.

UNINA9910703728303321

Autore

Jones Daniel S.

Titolo

Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]

Pubbl/distr/stampa


Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014

Descrizione fisica

1 online resource (25 pages) : color illustrations

Collana

NASA/TM ; ; 2014-218376

Soggetti

Convergent-divergent nozzles

Flow distribution

Inviscid flow

Nozzle design

Rocket nozzles

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

Title from title screen (viewed July 2, 2015).

"October 2014."

Nota di bibliografia

Includes bibliographical references (page 14).