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Preliminary Aerodynamic Shape Optimization of the SpaceLiner by Means of Engineering Methods

Neeb, Dominik and Schwanekamp, Tobias and Gülhan, Ali (2011) Preliminary Aerodynamic Shape Optimization of the SpaceLiner by Means of Engineering Methods. American Institute of Aeronautics and Astronautics. 17th AIAA International Space Planes and Hypersonic Systems and Technology Conference, 11-14 April 2011, San Francisco, USA.

Full text not available from this repository.

Abstract

An optimization routine has been implemented, validated and applied to improve the outer shape design of the DLR proposed SpaceLiner concept with engineering based aerodynamic tools including the estimation of aerothermodynamic loads. The routine consists of an aerodynamic approximation module based on Newtonian and additional engineering methods, a shape parameterization module to modify and mesh the geometry, and an optimization module based on a single-objective response surface methodology. The routine’s single components and the complete loop have been validated and tested to study their sensitivities. The optimization routine has been applied first to single components of the SpaceLiner to study sensitivities and influences of specific design parameters. Based on these studies the tool has been applied to the complete vehicle considering different flight conditions of a reference trajectory. The resulting shapes are evaluated for their longitudinal trim performance. An improvement in aerodynamic performance can be achieved especially in the hypersonic flow regime, which represents the major part of the trajectory.

Item URL in elib:https://elib.dlr.de/73939/
Document Type:Conference or Workshop Item (Paper)
Additional Information:AIAA-2011-2299
Title:Preliminary Aerodynamic Shape Optimization of the SpaceLiner by Means of Engineering Methods
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Neeb, DominikDLRUNSPECIFIED
Schwanekamp, TobiasDLRUNSPECIFIED
Gülhan, AliDLRUNSPECIFIED
Date:2011
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:American Institute of Aeronautics and Astronautics
Series Name:AIAA International Space Planes and Hypersonic Systems and Technology Conference
Status:Published
Keywords:SpaceLiner, Hypersonics, Aerodynamics, Optimization, Engineering method
Event Title:17th AIAA International Space Planes and Hypersonic Systems and Technology Conference
Event Location:San Francisco, USA
Event Type:international Conference
Event Dates:11-14 April 2011
Organizer:American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Neeb, Dominik
Deposited On:13 Jan 2012 08:33
Last Modified:13 Jan 2012 08:33

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