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High-Speed Compound Rotorcraft Performance and Design

Weiand, Peter and Atci, Kagan and Schwinn, Dominik (2024) High-Speed Compound Rotorcraft Performance and Design. In: 80th Annual Vertical Flight Society Forum and Technology Display, FORUM 2024. Vertical Flight Society's 80th Annual Forum & Technology Display, 2024-05-07 - 2024-05-09, Montreal, Kanada. ISBN 978-171389794-1.

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Abstract

High-speed configurations are among the new emerging concepts that are currently expanding the scope of rotorcraft design. Especially in the field of defense technology research, the capability of a substantial increase in maximum velocity becomes more interesting. For instance, NATO project NGRC is considering this capability for a new medium utility rotorcraft. DLR supports these activities by its continuing defense technology research. In this study the benefits and drawbacks of a high-speed capability for a given mission scenario are analyzed. For that purpose, a contemporary configuration has been modeled, featuring a maximum velocity of 82 m/s (160 KTAS). The high-speed configuration meets with the same mission requirements, but with an increase of about 50% of maximum speed to 125 m/s (242 KTAS). All tasks in this study are conducted with DLRs integrated design environment IRIS. The high-speed configuration features an off-loaded main rotor, a wing, a propeller and a reduction of the rotational speed of the drive train for the extended flight envelope. The reference configuration as well as the high-speed rotorcraft were compared with the focus on flight performance.

Item URL in elib:https://elib.dlr.de/204707/
Document Type:Conference or Workshop Item (Speech)
Title:High-Speed Compound Rotorcraft Performance and Design
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Weiand, PeterUNSPECIFIEDhttps://orcid.org/0000-0002-0964-6225UNSPECIFIED
Atci, KaganUNSPECIFIEDhttps://orcid.org/0000-0002-4975-4458175349237
Schwinn, DominikUNSPECIFIEDhttps://orcid.org/0000-0003-2341-9632UNSPECIFIED
Date:2024
Journal or Publication Title:80th Annual Vertical Flight Society Forum and Technology Display, FORUM 2024
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
ISBN:978-171389794-1
Status:Published
Keywords:Rotorcraft; Design; High-Speed Configuration; Compound Rotorcraft;
Event Title:Vertical Flight Society's 80th Annual Forum & Technology Display
Event Location:Montreal, Kanada
Event Type:international Conference
Event Start Date:7 May 2024
Event End Date:9 May 2024
Organizer:Vertical Flight Society
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Rotorcraft and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems
Institute of Structures and Design > Structural Integrity
Institute of Flight Systems > Rotorcraft
Deposited By: Weiand, Peter
Deposited On:09 Jan 2025 14:56
Last Modified:24 Feb 2025 09:47

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