Quantification of the Flap-Lag Coupling in Helicopter Rotors and How it Affects Piloted Simulations

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Original language	English
Title of host publication	Proceedings of the Internation Forum on Aeroelasticity and Structural Dynamics
Editors	s.n.
Place of Publication	Stockholm, Sweden
Publisher	KTH Vetensckap och Konst
Pages	1-15
Number of pages	15
Publication status	Published - 2007
Event	International Forum on Aeroelasticity and Structural Dynamics 2007 - Stockholm, Sweden Duration: 18 Jun 2007 → 20 Jun 2007

Name
Publisher	KTH Vetensckap och Konst

Conference	International Forum on Aeroelasticity and Structural Dynamics 2007
Period	18/06/07 → 20/06/07

Keywords

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title = "Quantification of the Flap-Lag Coupling in Helicopter Rotors and How it Affects Piloted Simulations",

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author = "MD Pavel",

year = "2007",

language = "English",

publisher = "KTH Vetensckap och Konst",

pages = "1--15",

editor = "s.n.",

booktitle = "Proceedings of the Internation Forum on Aeroelasticity and Structural Dynamics",

note = "International Forum on Aeroelasticity and Structural Dynamics 2007 ; Conference date: 18-06-2007 Through 20-06-2007",

}

Quantification of the Flap-Lag Coupling in Helicopter Rotors and How it Affects Piloted Simulations. / Pavel, MD.
Proceedings of the Internation Forum on Aeroelasticity and Structural Dynamics. ed. / s.n. Stockholm, Sweden: KTH Vetensckap och Konst, 2007. p. 1-15.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - Quantification of the Flap-Lag Coupling in Helicopter Rotors and How it Affects Piloted Simulations

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PY - 2007

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M3 - Conference contribution

SP - 1

EP - 15

BT - Proceedings of the Internation Forum on Aeroelasticity and Structural Dynamics

A2 - s.n., null

PB - KTH Vetensckap och Konst

CY - Stockholm, Sweden

T2 - International Forum on Aeroelasticity and Structural Dynamics 2007

Y2 - 18 June 2007 through 20 June 2007

ER -