Skip to main content
Disciplines
Automotive Business IT + Informatics Construction + Real Estate Electrical Engineering + Electronics Energy + Sustainability Insurance + Risk Finance + Banking Management + Leadership Marketing + Sales Mechanical Engineering + Materials
Events
DE
EN
Books
Journals
Topic Page
Marketing
Start single access now
Access for companies
EXTENDED SEARCH
Log in
Top
Published in:
Unconventional Applications and New Approaches for Flow Control Read chapter Read first chapter

2021 | OriginalPaper | Chapter

Aerodynamic Optimization of the OWN Configurations REF3 and REF4 in Cruise Flight

Authors : Fabian Lange, Ralf Rudnik

Published in: Fundamentals of High Lift for Future Civil Aircraft

Publisher: Springer International Publishing

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

Detailed investigations of interference effects between over-the-wing mounted nacelles (OWN) and airframe were accomplished with the aid of high-fidelity CFD tools on two aircraft configurations. The configurations differ in a variation of the wing planform from a backward (REF3) to a forward swept layout (REF4). The impact of the OWN was investigated by using an automated process chain varying engine position, wing twist distribution, and airfoil section geometry to achieve an aerodynamically efficient aircraft design in the presence of the OWN. Ensuing from the surrogate-based optimization, the data set was used to evaluate the interference between OWN and wing.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

inform now
previous chapter Aerodynamics and Loss Accounting of a Low Pressure Ratio Fan for an Over-Wing Mounted Engine
next chapter Intake Design and Airframe Integration Sensitivities for an Embedded Over-The-Wing Mounted Ultra-High Bypass Ratio Turbofan
Literature
1.
Allmaras, S.R., Johnson, F.T., Spalart, P.R.: Modification and clarifications for the implementation of the spalartallmaras turbulence model. In: 7th International Conference on Computational Fluid Dynamics ICCFD7-1902 (2012)
2.
Delfs, J., Appel, C., Bernicke, P., Blech, C., Blinstrub, J., Heykena, C., Kumar, P., Kutscher, K., Lippitz, N., Rossian, L., Savoni, L., Lummer, M.: Aircraft and technology for low noise short take-off and landing
3.
Destarac, D., van der Vooren, J.: Drag/thrust analysis of jet-propelled transonic transport aircraft; Definition of physical drag components. Aerosp. Sci. Technol. 8, 545–556 (2004)CrossRefMATH
4.
Gerhold, T.: Overview of the Hybrid Rans Code TAU. Megaflow—Numerical Flow Simulation for Aircraft Design, pp. 81–92 (2005)
5.
Giesecke, D., Lehmler, M., Friedrichs, J., Blinstrub, J., Bertsch, L., Heinze, W.: Evaluation of ultra-high bypass ratio engines for an over-wing aircraft configuration 2, 493–515, 10 (2018)
6.
Heinze, W.: Main Data Sheet. A/C Type: REF3-2015 basis (with improvements in the second CRC 880 period 2015-2018) (2017)
7.
Heinze, W.: Main Data Sheet. A/C Type: SFB880 Reference Aircraft REF4-2019 FSW (2019)
8.
D. Keller and R. Rudnik. Configurational Aspects of a Circulation Controlled High-Lift System for a Medium-Haul Transport Aircraft. DLRK, 2019
9.
Krige, D.: A statistical approach to some mine valuation and allied problems on the Witwatersrand. Ph.D. thesis (1951)
10.
Lange, F.: High fidelity design of the AVACON research baseline aircraft based on CPACS data set. In: 54th 3AF International Conference on Applied Aerodynamics (2019)
11.
Lange, F., Rudnik, R.: Wing Shape Improvement in the Presence of an Over-the-wing Mounted UHBR Engine for a Short Range Transport Aircraft. AIAA paper (2019)
12.
Renganathan, A., Berguin, S.H., Chen, M., Ahuja, J., Tai, J.C., Mavris, D.N., Hills, D.: Sensitivity analysis of aero-propulsive coupling for over-wing-nacelle concepts. In: 2018 AIAA Aerospace Sciences Meeting (2018)
13.
Ronzheimer, A.: CAD-centric aircraft design. In: 7th European Conference on Computational Fluid Dynamics (ECFD 7) (2018)
14.
Rudnik, R., Melber-Wilkending, S., Risley-Settle, P.: TAU-SOLAR Contribution to the 3rd High Lift Prediction Workshop. AIAA Paper (2018)
15.
Spalart, P.R., Allmaras, S.R.: A One-Equation Turbulence Model for Aerodynamic Flows. AIAA Paper (1992)
16.
Wilke, G.A.: Aerodynamic Optimization of Helicopter Rotor Blades using Variable Fidelity Methods. Ph.D. thesis (2017)
Metadata
Title
Aerodynamic Optimization of the OWN Configurations REF3 and REF4 in Cruise Flight
Authors
Fabian Lange
Ralf Rudnik
Copyright Year
2021
Book
Fundamentals of High Lift for Future Civil Aircraft

Print ISBN: 978-3-030-52428-9

Electronic ISBN: 978-3-030-52429-6

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-3-030-52429-6_20

Premium Partners

    Image Credits