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Aerodynamic Measurements of an Air-Breathing Hypersonic Vehicle at Mach 3.5 to 8

Gruhn, Patrick and Gülhan, Ali (2018) Aerodynamic Measurements of an Air-Breathing Hypersonic Vehicle at Mach 3.5 to 8. AIAA Journal, 56 (11), pp. 4282-4296. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J056522. ISSN 0001-1452.

Full text not available from this repository.

Official URL: http://dx.doi.org/10.2514/1.J056522

Abstract

Six-degree-of-freedom measurements have been performed with an aerodynamic model of a small scale hypersonic air-breathing vehicle. The model was tested in two test campaigns in two different wind tunnels, with Mach numbers ranging from the supersonic to the hypersonic range (Mach 3.5 to Mach 8). The tests included variations of the angle of attack between α = -3° and α = 3°, and of the sideslip angle between β = 0° and β = 2°. Further on, various control surface deflections have been set for canards, rudders and ailerons. The experiments provided insight into the aerodynamic properties and gave valuable information for the design of the vehicle. Further on they provided validation data for planned nose-to-tail computations of the vehicle.

Item URL in elib:https://elib.dlr.de/121985/
Document Type:Article
Title:Aerodynamic Measurements of an Air-Breathing Hypersonic Vehicle at Mach 3.5 to 8
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Gruhn, PatrickPatrick.Gruhn (at) dlr.deUNSPECIFIED
Gülhan, AliAli.Guelhan (at) dlr.dehttps://orcid.org/0000-0003-4905-5881
Date:11 November 2018
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:56
DOI :10.2514/1.J056522
Page Range:pp. 4282-4296
Editors:
EditorsEmailEditor's ORCID iD
UNSPECIFIEDAIAAUNSPECIFIED
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0001-1452
Status:Published
Keywords:hypersonic air-breathing Propulsion
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
Location: Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonoc and Hypersonic Technology
Deposited By: Gruhn, Patrick
Deposited On:17 Oct 2018 12:42
Last Modified:20 Jun 2021 15:51

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