Defining gas turbine engine performance requirements for the Large Civil TiltRotor (LCTR2) /

Bibliographic Details

Main Author:	Snyder, Christopher A. (Author)
Corporate Author:	Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
Series:	NASA technical memorandum ; 218101.
Subjects:	Tilt rotor aircraft. Rotary wing aircraft. Gas turbine engines. Rotor speed. Vertical takeoff. Tilting rotors.
Online Access:	https://purl.fdlp.gov/GPO/gpo53695 http://purl.fdlp.gov/GPO/gpo53695