elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

An Experimental Study of Chin-Intakes for Airbreathing Missiles with High Agility

Herrmann, Dirk and Triesch, Klaus and Gülhan, Ali (2007) An Experimental Study of Chin-Intakes for Airbreathing Missiles with High Agility. Journal of Propulsion and Power, 24 (2), pp. 236-244. AIAA.

Full text not available from this repository.

Abstract

The performance of three chin-intakes for airbreathing missiles with high agility has been investigated in a large maneuver range at supersonic speed. This experimental study is recovery and mass flow were discovered at angles of attack greater than 18°. To understand these effects in more details chin-intakes have been analyzed at a design Mach number of 3.0 at angles of attack ranging from -30° to 30° and at angles of sideslip ranging from -30° and 30° in the Trisonic Wind Tunnel. The results clearly show that boundary layer flow, vortices and flow sepration are responsible for the losses of pressure recovery and mass flow. The subsequently added boundary layer bleed permits a better pressure recovery and a delay of the intake buzzing.

Item URL in elib:https://elib.dlr.de/52392/
Document Type:Article
Title:An Experimental Study of Chin-Intakes for Airbreathing Missiles with High Agility
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Herrmann, DirkUNSPECIFIEDUNSPECIFIED
Triesch, KlausUNSPECIFIEDUNSPECIFIED
Gülhan, AliUNSPECIFIEDUNSPECIFIED
Date:2007
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:24
Page Range:pp. 236-244
Publisher:AIAA
Series Name:Journal of Propulsion and Power
Status:Published
Keywords:missiles, air breathing propulsion, high agility, ramjet performance
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - no assignment (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By:INVALID USER
Deposited On:26 Mar 2008
Last Modified:15 Jan 2010 02:06

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.