NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Validation of an Integrated Airframe and Turbofan Engine Simulation for Evaluation of Propulsion Control ModesThe National Aeronautics and Space Administration (NASA) has developed independent airframe and engine models that have been integrated into a single real-time aircraft simulation for piloted evaluation of propulsion control algorithms. In order to have confidence in the results of these evaluations, the integrated simulation must be validated to demonstrate that its behavior is realistic and that it meets the appropriate Federal Aviation Administration (FAA) certification requirements for aircraft. The paper describes the test procedures and results, demonstrating that the integrated simulation generally meets the FAA requirements and is thus a valid testbed for evaluation of propulsion control modes.
Document ID
20150002109
Document Type
Conference Paper
Authors
Litt, Jonathan (NASA Glenn Research Center Cleveland, OH United States)
Sowers, T Shane (Vantage Partners, LLC Brook Park, OH, United States)
Liu, Yuan (N and R Engineering and Management Services Parma Heights, OH, United States)
Owen, A. Karl (Owen (A. Karl) Consultant North Royalton, OH, United States)
Guo, Ten-Huei (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 25, 2015
Publication Date
January 5, 2015
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
GRC-E-DAA-TN19726
Meeting Information
SciTech 2015(Kissimmee, FL)
Funding Number(s)
CONTRACT_GRANT: NNC10BA16B
WBS: WBS 284848.02.50.03
CONTRACT_GRANT: NNC12BA01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
aircraft engine simulation
emergency operation
aircraft engine performance

Available Downloads

NameType 20150002109.pdf STI