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SHEFEX II - An Aerodynamic and Structural Post-Flight Analysis

Franze, Marius (2016) SHEFEX II - An Aerodynamic and Structural Post-Flight Analysis. In: AIAA Atmospheric Flight Mechanics Conference, 2016. AIAA Atmospheric Flight Mechanics Conference, 2016-06-13 - 2016-06-17, Washington D.C., USA. doi: 10.2514/6.2016-3237.

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Abstract

This work is subsequent to the aerodynamic and atmospheric analysis presented in an earlier paper, which presumed a structural deformation of the main fins of SHEFEX II. For this reason the ascend phase of the vehicle is analyzed to get the maximum surface loads of the fins. Later, the extracted pressure loads where applied to a high fidelity structural model for a static analysis. The structural model consists of the tailcan, including its stringer and rib parts, and the in detail modeled fins. Overall the predicted fin deformation got confirmed, which means that the fin control impact reduces to the shown roll rate plots.

Item URL in elib:https://elib.dlr.de/105015/
Document Type:Conference or Workshop Item (Speech)
Title:SHEFEX II - An Aerodynamic and Structural Post-Flight Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Franze, MariusUNSPECIFIEDhttps://orcid.org/0000-0002-7706-098XUNSPECIFIED
Date:June 2016
Journal or Publication Title:AIAA Atmospheric Flight Mechanics Conference, 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2016-3237
Status:Published
Keywords:flight mechanic; structure; atmosphere; unsteady aerodynamics; shefex
Event Title:AIAA Atmospheric Flight Mechanics Conference
Event Location:Washington D.C., USA
Event Type:international Conference
Event Start Date:13 June 2016
Event End Date:17 June 2016
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 - Shefex III (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Franze, Marius
Deposited On:05 Jul 2016 09:52
Last Modified:24 Apr 2024 20:10

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