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SHEFEX — A First Aerodynamic Post-flight Analysis

  • Tarik Barth
  • Thino Eggers
Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM) book series (NNFM, volume 96)

Abstract

The given paper summarises the status of the post-flight analysis of the SHarp Edge Flight EXperiment (SHEFEX). It focuses on the comparison of numerical and experimental surface pressures as well as the assessment of the free stream vector applying the flight mechanic description of the Digital Miniature Attitude Reference System (DMARS) platform. The results point out that the extraction of angles of attack and sideslip is much more demanding than expected.

Keywords

Mach Number Roll Angle Sideslip Angle Mechanic Description Thermal Protection System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    Digital Dutch: The 1976 Standard Atmosphere, http: //digitaldutch.com.Google Scholar
  2. [2]
    Giilhan, A.; Requardt, G.; Siebe, F.; Koch, U.; Esser, B.: Instrumentation and In-Flight Data of the SHEFEX Flight Experiment. Proceedings of the 1st International ARA Days on Atmospheric Re-Entry Systems, Missions and Vehicles, Arcachon, France, June 2006Google Scholar
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    Longo, J.M.A.: Aerothermodynamics A critical review at DLR. Aerosp. Sci. Technol. 7 (2003) 429–438.zbMATHCrossRefGoogle Scholar
  4. [4]
    Turner, J.; Hörschgen, M.; Stamminger, A.; Turner, P.: SHEFEX Hypersonic Reentry Flight Experiment, Vehicle and Subsystem Design, Flight Performance and Prospects. AIAA Paper 2006–8115, 2006.Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 2007

Authors and Affiliations

  • Tarik Barth
    • 1
  • Thino Eggers
    • 1
  1. 1.DLRInstitute of Design AerodynamicsBraunschweigGermany

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