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Derivation of a Helicopter Engine and Rotor Governing System Model Using Flight Test Data

Ehrsam, Adrian (2008) Derivation of a Helicopter Engine and Rotor Governing System Model Using Flight Test Data. DLR-Interner Bericht. DLR-IB 111-2008/11, 117 S.

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Item URL in elib:https://elib.dlr.de/62633/
Document Type:Monograph (DLR-Interner Bericht)
Title:Derivation of a Helicopter Engine and Rotor Governing System Model Using Flight Test Data
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ehrsam, AdrianUNSPECIFIEDUNSPECIFIED
Date:2008
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:117
Status:Published
Keywords:Modellierung, Hubschrauber, Triebwerk, Regelung
Institution:Cranfield University
Department:School of Engineering
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Smart Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: Grünhagen, Dr.-Ing. Wolfgang
Deposited On:10 Feb 2010 15:24
Last Modified:10 Feb 2010 15:24

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