Skip to main content
SpringerLink
Log in

Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration

  • Conference paper
  • First Online:
Advances in Simulation of Wing and Nacelle Stall (FOR 1066 2014)

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 131))

Included in the following conference series:

  • 1780 Accesses

Abstract

Within the German national research project HINVA (High-lift INflight VAlidation) the prediction of maximum lift of realistic transport aircraft configurations shall be improved. This is achieved by a close link of flight tests, cryogenic wind tunnel tests and numerical simulations. Within the HINVA flight test campaign in 2012 several so called pressure belts were installed on one wing of the Airbus A320 used for the flight tests to measure surface pressure data on the wing for the complete polar up to \(C_{Lmax}\). To investigate the influence of these belts on the measured data, a numerical investigation was performed. This paper will show the results of these investigations by a comparison of simulations with and without pressure belts.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Log in via an institution
Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 169.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Hardcover Book
USD 219.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Bier, N., Keye, S., Rohlmann, D.: Design of a Wind Tunnel Model for Maximum Lift Predictions Based on Flight Test Data. In: AIAA Paper, pp. 2013–2930. AIAA (2013)

    Google Scholar 

  2. Bier, N., Rohlmann, D., Rudnik, R.: Numerical Maximum Lift Predictions of a Realistic Commercial Aircraft in Landing Configuration. In: AIAA Paper, pp. 2012–0279. AIAA (2012)

    Google Scholar 

  3. CentaurSoft. http://www.centaursoft.com (2014)

  4. Gerhold, T.: Overview of the Hybrid RANS Code TAU. In: Kroll, N., Fassbender, J. (eds.) MEGAFLOW. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 89, pp. 81–92. Springer (2005)

    Google Scholar 

  5. Keye, S., Rohlmann, D.: Aeroelasic Effects in Maximum Lift Prediction of a Transport Aircraft and Comparison to Flight Data. In: AIAA Paper, pp. 2014–2842. AIAA (2014)

    Google Scholar 

  6. Nallapula, V., Bier, N., Rohlmann, D., Radespiel, R.: Simulation of the Horizontal Tail Plane Stall of a Transport Aircraft. AIAA Paper, pp. 2012–3142. AIAA (2012)

    Google Scholar 

  7. Rudnik, R., Reckzeh, D., Quest, J.: HINVA - High lift INight VAlidation - Project Overview and Status. In: AIAA Paper, pp. 2012–0106. AIAA (2012)

    Google Scholar 

  8. Rudnik, R., Schwetzler, D.: High lift INflight VAlidation (HINVA) - Overview about the 1st Flight Test Campaign. In: AIAA Paper, pp. 2014–2843. AIAA (2014)

    Google Scholar 

  9. Spalart, P., Allmaras, S.: A One-Equation Turbulence Model for Aerodynamic Flows. In: AIAA Paper, pp. 1992–439 (1992)

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. DLR, Institute of Aerodynamics and Flow Technology, Lilienthalplatz 7, 38108, Braunschweig, Germany

    David Rohlmann

Authors
  1. David Rohlmann
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to David Rohlmann .

Editor information

Editors and Affiliations

  1. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Rolf Radespiel

  2. Institute of Jet Propulsion, Universität der Bundeswehr München, Neubiberg, Germany

    Reinhard Niehuis

  3. Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Braunschweig, Germany

    Norbert Kroll

  4. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Kathrin Behrends

Rights and permissions

Reprints and permissions

Copyright information

© 2016 Springer International Publishing Switzerland

About this paper

Cite this paper

Rohlmann, D. (2016). Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration. In: Radespiel, R., Niehuis, R., Kroll, N., Behrends, K. (eds) Advances in Simulation of Wing and Nacelle Stall. FOR 1066 2014. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 131. Springer, Cham. https://doi.org/10.1007/978-3-319-21127-5_23

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-21127-5_23

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-21126-8

  • Online ISBN: 978-3-319-21127-5

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics

Search

Navigation