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Dependence of liquid oxygen core length on transverse acoustic amplitude for shear coaxial injection in a rocket combustion chamber

Satish Babu, J. P. (2019) Dependence of liquid oxygen core length on transverse acoustic amplitude for shear coaxial injection in a rocket combustion chamber. Master's, Indian Institute of Technology, Kharagpur, India.

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Item URL in elib:https://elib.dlr.de/132953/
Document Type:Thesis (Master's)
Title:Dependence of liquid oxygen core length on transverse acoustic amplitude for shear coaxial injection in a rocket combustion chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Satish Babu, J. P.DLR, Inst. für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Date:2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:134
Status:Published
Keywords:LOX, acoustic, rocket combustion chamber
Institution:Indian Institute of Technology, Kharagpur, India
Department:Department of Aerospace Engineering
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2019 16:07
Last Modified:18 Dec 2019 16:07

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