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Aeroelastic Investigations on High-Altitude Research Aircraft Strato 2C.

Kießling, F. and Rippl, M. (1995) Aeroelastic Investigations on High-Altitude Research Aircraft Strato 2C. International Forum on Aeroelasticity and Structural Dynamics 1995, 26-28 June, Manchester, UK..

Full text not available from this repository.

Abstract

The STRATO 2C aircraft is currently being developed for manned stratospheric research missions up to 80,000 ft. It is powered by two 330 kW turbocharged piston engines. The requirements for flight endurance, altitude, payload, and operating range can only be met if high aerodynamic quality, high propulsion efficiency, and low empty weight are achieved simultaneously. The large wing span (56.5m) and aspect ratio (21.3) result from aerodynamic optimization. Carbon fibre composites are applied to reduce weight and deflections. Possible aeroelastic problems are dealt with during aircraft deve- lopment. This paper gives an overview on these activities.

Item URL in elib:https://elib.dlr.de/39714/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1995,
Title:Aeroelastic Investigations on High-Altitude Research Aircraft Strato 2C.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kießling, F.UNSPECIFIEDUNSPECIFIED
Rippl, M.UNSPECIFIEDUNSPECIFIED
Date:1995
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:aeroelasticity, flutter, High-Altitude Research Aircraft.
Event Title:International Forum on Aeroelasticity and Structural Dynamics 1995, 26-28 June, Manchester, UK.
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:52

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