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Performance studies on the application of four-engine and two-engine USB propulsive lift to the E-2C aircraftA study has been completed of the performance benefits to be derived from applying advanced upper-surface blowing (USB) propulsive-lift technology to the E-2C aircraft. The results of comparing four-engine with two-engine USB configurations are discussed, and engine sizing and aerodynamic/structural considerations pertaining to the E-2C/USB modification are examined. The effects of the modification on performance are described in detail with regard to takeoff distance and landing distance estimation in free-deck operations, operations using catapult and arresting gear, ceiling and radar surveillance missions, and range and endurance capability.
Document ID
19870030641
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riddle, D. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Stevens, V. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-2674
Accession Number
87A17915
Distribution Limits
Public
Copyright
Other

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