Defining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2) / / Christopher A. Snyder

• Autore: Snyder Christopher A.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
• Descrizione fisica: 1 online resource (10 pages) : color illustrations
• Soggetto topico: Tilt rotor aircraft; Rotary wing aircraft; Gas turbine engines; Rotor speed; Vertical takeoff; Tilting rotors
• Note generali: Title from title screen (viewed on Dec. 3, 2014).; "December 2013."; "Prepared for the 67th Annual Forum and Technology Display (FORUM 67) sponsored by the American Helicopter Society International (AHS), Virginia Beach, Virginia, May 3-5, 2011."
• Nota di bibliografia: Includes bibliographical references (page 10).
• Altri titoli varianti: Defining gas turbine engine performance requirements for the Large Civil TiltRotor
• Titolo autorizzato: Defining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2)
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910702508303321
• Lo trovi qui: Univ. Federico II