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Low Speed Experimental and Numerical Investigations on Unconventional Control Concepts for Agile and Highly Swept Aircraft Configurations

Paul, Michael (2015) Low Speed Experimental and Numerical Investigations on Unconventional Control Concepts for Agile and Highly Swept Aircraft Configurations. 17. STAB-Workshop, 2015-11-10 - 2015-11-11, Göttingen, Deutschland.

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Official URL: http://www.dlr.de/agstab

Abstract

The use of delta and lambda wing configurations has increased in recent years as the reliance on Unmanned Combat Air Vehicles (UCAV) has surged. The tailless lambda wing configuration is desirable for its stealth characteristics and natural aerodynamic efficiency, but poses significant stability and control challenges. Future UCAVs will need to achieve stealth perfonmance as well as high maneuverability, two factors which directly oppose each other due to the stealth penalty of traditional control surfaces.

Item URL in elib:https://elib.dlr.de/99864/
Document Type:Conference or Workshop Item (Speech)
Title:Low Speed Experimental and Numerical Investigations on Unconventional Control Concepts for Agile and Highly Swept Aircraft Configurations
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Paul, MichaelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 104-105
Series Name:Jahresbericht 2015, STAB-Mitteilung
Status:Published
Keywords:Unmanned Combat Air Vehicles (UCAV), Highly Swept Aircraft, Low Speed Experimental
Event Title:17. STAB-Workshop
Event Location:Göttingen, Deutschland
Event Type:Workshop
Event Start Date:10 November 2015
Event End Date:11 November 2015
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Micknaus, Ilka
Deposited On:07 Dec 2015 16:22
Last Modified:24 Apr 2024 20:05

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