Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Launchers aeroelastic analysis in early-phase development
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Flight Dynamics.
2018 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

This paper accounts for the work performed during the Degree Project for the Master’s Programme in Aerospace Engineering. It provides an aeroelastic study of launchers in Pre-Study. During this phase, the geometry is too coarse and design parameters too scarce to perform a CFD analysis. The objective is to elaborate the simplest yet most accurate method to anticipate the aeroelastic behaviour of a new launcher. A reference diagram was thus built based on a simple geometric parameter and on the architectures of existing launchers. This diagram is accurate and simple enough to be used in preliminary phase projects.

Abstract [sv]

Det dokumentet sammanfattar verksamheten som utfördes på Examensarbetet för det Master’s Programme in Aerospace Engineering. Det ger en aeroelastisk analys av en raket på för-studie. Medan den fasen är geometrin alltför grov för att genomföra en CFD analys. Så är målet att utveckla den enklaste dock mest precis metoden för att förutse raketens aeroelastisk beteende. En referensdiagram är då byggnad med en enkel geometrisk parameter och raketer som redan finns. Det diagrammet är nog precist och enklet för att användas i kommande projekt.

Place, publisher, year, edition, pages
2018. , p. 11
Series
TRITA-SCI-GRU ; 2018:324
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-244828OAI: oai:DiVA.org:kth-244828DiVA, id: diva2:1292387
External cooperation
CNES
Examiners
Available from: 2019-02-28 Created: 2019-02-28 Last updated: 2019-02-28Bibliographically approved

Open Access in DiVA

No full text in DiVA

By organisation
Flight Dynamics
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar

urn-nbn

Altmetric score

urn-nbn
Total: 39 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf