Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner

• Autore: Castner Raymond S
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
• Descrizione fisica: 1 online resource (16 pages) : color illustrations
• Soggetto topico: Exhaust nozzles; Sonic booms; Computational fluid dynamics; Elastic waves; Plumes; F-15 aircraft; Supersonic aircraft; Pressure ratio
• Note generali: Title from title screen (viewed on Nov. 1, 2012).; "February 2012."; "Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE,San Diego, California, July 31-August 3, 2011."; "AIAA-2011-5974."
• Nota di bibliografia: Includes bibliographical references (pages 15-16).
• Titolo autorizzato: Exhaust nozzle plume effects on sonic boom test results for vectored nozzles
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910701950003321
• Lo trovi qui: Univ. Federico II