Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles

Schneider, Dirk and Génin, C. (2015) Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles. In: 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015. 51st AIAA Joint Propulsion Conference, 2015-07-27 - 2015-07-29, Orlando, FL, USA. doi: 10.2514/6.2015-4219.

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Item URL in elib:

https://elib.dlr.de/99609/

Document Type:

Conference or Workshop Item (Speech)

Title:

Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Schneider, Dirk	UNSPECIFIED	https://orcid.org/0000-0002-4785-4244	UNSPECIFIED
Génin, C.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2015

Journal or Publication Title:

51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

DOI:

10.2514/6.2015-4219

Status:

Published

Keywords:

dual bell nozzle, flow separation, altitude adaptive nozzles, nozzle flow

Event Title:

51st AIAA Joint Propulsion Conference

Event Location:

Orlando, FL, USA

Event Type:

international Conference

Event Start Date:

27 July 2015

Event End Date:

29 July 2015

Organizer:

AIAA

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transportation

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Space Transportation

DLR - Research theme (Project):

R - ProTAU + Prop2020 Hochleistungstriebwerke (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion

Deposited By:

Hanke, Michaela

Deposited On:

20 Nov 2015 09:13

Last Modified:

24 Apr 2024 20:05

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