Skip to main content
Top

2021 | OriginalPaper | Chapter

Understanding the Flight Mechanics of Active High-Lift Aircraft Configurations: Achievements of the CRC 880 Project

Authors : Yannic Beyer, Jobst H. Diekmann, Nicolas Fezans, Meiko Steen

Published in: Fundamentals of High Lift for Future Civil Aircraft

Publisher: Springer International Publishing

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

search-config
loading …

Abstract

Flight mechanics of short take-off and landing aircraft with active high-lift system and propeller engines exhibit excellent low airspeed flight performance on the one hand but also flight mechanical challenges on the other. These are results of previous work of the 60s as well as of the Collaborative Research Centre CRC 880. In the CRC 880 project, new knowledge about unsatisfactory handling qualities was gained by flight dynamics modeling and simulations based on a high-fidelity computational fluid dynamics database of the CRC reference aircraft. This paper summarizes the results of the flight dynamics that confirm excellent flight performance, minor challenges in the longitudinal motion and major challenges in the lateral-directional motion. Passive and active countermeasures are discussed to improve the handling qualities. Moreover, it is shown that only partial failures of the active high-lift system can be compensated. Finally, the paper gives an outlook on future work.

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!

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!

Footnotes
1
Note that an intermediate configuration would be a preferable first action but no data on intermediate flaps configurations was available at the time of this investigation.
 
Literature
3.
go back to reference Cook, W.L., Holzhauser, C.A., Kelly, M.W.: The use of area suction for the purpose of improving trailing-edge flap effectiveness on a 35\(^\circ \) sweptback wing. Research Memorandum A53E06, NACA (1953) Cook, W.L., Holzhauser, C.A., Kelly, M.W.: The use of area suction for the purpose of improving trailing-edge flap effectiveness on a 35\(^\circ \) sweptback wing. Research Memorandum A53E06, NACA (1953)
4.
go back to reference Kelly, M.W., Tolhurst, W.H.: Full-scale wind-tunnel tests of a 35\(^\circ \) sweptback wing airplane with high-velocity blowing over the trailing-edge flaps. Research Memorandum A55I09, NACA (1955) Kelly, M.W., Tolhurst, W.H.: Full-scale wind-tunnel tests of a 35\(^\circ \) sweptback wing airplane with high-velocity blowing over the trailing-edge flaps. Research Memorandum A55I09, NACA (1955)
5.
go back to reference Kuhn, R.E., Draper, J.W.: Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90\(^\circ \). Report 1263, NACA (1956) Kuhn, R.E., Draper, J.W.: Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90\(^\circ \). Report 1263, NACA (1956)
6.
go back to reference Weiberg, J.A., Page, V.R.: Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps. Technical Note D-25, NASA (1959) Weiberg, J.A., Page, V.R.: Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing, four propellers, and blowing flaps. Technical Note D-25, NASA (1959)
7.
go back to reference Holzhauser, C.A., Innis, R.C., Vomaske, R.F.: A flight and simulator study of the handling qualities of a deflected slipstream STOL seaplane having four propellers and boundary-layer control. Technical Note D-2966, NASA (1965) Holzhauser, C.A., Innis, R.C., Vomaske, R.F.: A flight and simulator study of the handling qualities of a deflected slipstream STOL seaplane having four propellers and boundary-layer control. Technical Note D-2966, NASA (1965)
8.
go back to reference Innis, R.C., Quigley, H.C.: A flight examination of operating problems of V/STOL aircraft in stol-type landing and approach. Technical Note D-862, NASA (1961) Innis, R.C., Quigley, H.C.: A flight examination of operating problems of V/STOL aircraft in stol-type landing and approach. Technical Note D-862, NASA (1961)
9.
go back to reference Quigley, H.C., Innis, R.C.: Handling qualities and operational problems of a large four-propeller STOL airplane. Technical Note D-1647, NASA (1963) Quigley, H.C., Innis, R.C.: Handling qualities and operational problems of a large four-propeller STOL airplane. Technical Note D-1647, NASA (1963)
10.
go back to reference Rolls, L.S., Innis, R.C.: Flight evaluation of a wing-shroud-blowing boundary-layer control system applied to the flaps of an F9F-4 airplane. Research Memorandum 55K01, NACA (1955) Rolls, L.S., Innis, R.C.: Flight evaluation of a wing-shroud-blowing boundary-layer control system applied to the flaps of an F9F-4 airplane. Research Memorandum 55K01, NACA (1955)
11.
go back to reference Garren, J.F., Kelly, J.R., Reeder, J.P.: Effects of gross changes in static directional stability on V/STOL handling characteristics based on a flight investigation. Technical Note D-2477, NASA (1964) Garren, J.F., Kelly, J.R., Reeder, J.P.: Effects of gross changes in static directional stability on V/STOL handling characteristics based on a flight investigation. Technical Note D-2477, NASA (1964)
12.
go back to reference Quigley, H.C., Lawson, H.F.: Simulator study of the lateral-directional handling qualities of a large four-propellered STOL transport airplane. Technical Note D-1773, NASA (1963) Quigley, H.C., Lawson, H.F.: Simulator study of the lateral-directional handling qualities of a large four-propellered STOL transport airplane. Technical Note D-1773, NASA (1963)
13.
go back to reference Quigley, H.C., Innis, R.C., Vomaske, R.F., Ratcliff, J.W.: A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane. Technical Note D-3909, NASA (1967) Quigley, H.C., Innis, R.C., Vomaske, R.F., Ratcliff, J.W.: A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane. Technical Note D-3909, NASA (1967)
14.
go back to reference Henri, C.: Device for deflecting a stream of elastic fluid projected into an elastic fluid (1936). US Patent 2,052,869 Henri, C.: Device for deflecting a stream of elastic fluid projected into an elastic fluid (1936). US Patent 2,052,869
17.
go back to reference Diekmann, J.H.: Flugmechanische Charakteristika von propellergetriebenen Flugzeugen mit aktiven Hochauftriebssystemen. Dissertation., TU Braunschweig (2017). DLR-Forschungsbericht. ISSN 1434-8454, ISRN DLR-FB-2017-54 Diekmann, J.H.: Flugmechanische Charakteristika von propellergetriebenen Flugzeugen mit aktiven Hochauftriebssystemen. Dissertation., TU Braunschweig (2017). DLR-Forschungsbericht. ISSN 1434-8454, ISRN DLR-FB-2017-54
19.
go back to reference Keller, D., Rudnik, R.: Integration aspects of lift augmentation systems on the aerodynamics of a high-lift configuration. In: Radespiel, R., Semaan, R. (eds.) SFB 880—Fundamentals of high-lift for future commertial aircraft. Biennial Report. TU Braunschweig—Campus Forschungsflughafen, Braunschweig (2015). ISBN 978-3-928628-67-9 Keller, D., Rudnik, R.: Integration aspects of lift augmentation systems on the aerodynamics of a high-lift configuration. In: Radespiel, R., Semaan, R. (eds.) SFB 880—Fundamentals of high-lift for future commertial aircraft. Biennial Report. TU Braunschweig—Campus Forschungsflughafen, Braunschweig (2015). ISBN 978-3-928628-67-9
21.
go back to reference Beyer, Y., Kuzolap, A., Steen, M., Diekmann, J.H., Fezans, N.: Adaptive nonlinear flight control of stol-aircraft based on incremental nonlinear dynamic inversion. In: 2018 Modeling and Simulation Technologies Conference, AIAA 2018-3257 (2018). https://doi.org/10.2514/6.2018-3257 Beyer, Y., Kuzolap, A., Steen, M., Diekmann, J.H., Fezans, N.: Adaptive nonlinear flight control of stol-aircraft based on incremental nonlinear dynamic inversion. In: 2018 Modeling and Simulation Technologies Conference, AIAA 2018-3257 (2018). https://​doi.​org/​10.​2514/​6.​2018-3257
23.
go back to reference MIL-HDBK-1797A. Flying qualities of piloted aircraft. Military Handbook, Department of Defense (1997) MIL-HDBK-1797A. Flying qualities of piloted aircraft. Military Handbook, Department of Defense (1997)
24.
go back to reference Anderson, S.B., Chinn, H.W., Filisetti, A., Hafer, X., McGregor, D.M., Schroers, L.G., Ville, G.: V/stol handling. Report AGARD-R-577-70, Advisory Group for Aerospace Research and Development, NATO (1970) Anderson, S.B., Chinn, H.W., Filisetti, A., Hafer, X., McGregor, D.M., Schroers, L.G., Ville, G.: V/stol handling. Report AGARD-R-577-70, Advisory Group for Aerospace Research and Development, NATO (1970)
25.
go back to reference Hefferley, R.K., Stapleford, R.L., Rumold, R.C.: Airworthiness criteria development for powered-lift aircraft. Contractor Report NASA CR-2791 / FAA-RD-76-195, NASA/FAA (1977) Hefferley, R.K., Stapleford, R.L., Rumold, R.C.: Airworthiness criteria development for powered-lift aircraft. Contractor Report NASA CR-2791 / FAA-RD-76-195, NASA/FAA (1977)
27.
go back to reference Diekmann, J.H.: Investigation of flight dynamics of a civil aircraft with active high lift system. In: Deutscher Luft- und Raumfahrtkongress 2012. Berlin, Germany (2012) Diekmann, J.H.: Investigation of flight dynamics of a civil aircraft with active high lift system. In: Deutscher Luft- und Raumfahrtkongress 2012. Berlin, Germany (2012)
Metadata
Title
Understanding the Flight Mechanics of Active High-Lift Aircraft Configurations: Achievements of the CRC 880 Project
Authors
Yannic Beyer
Jobst H. Diekmann
Nicolas Fezans
Meiko Steen
Copyright Year
2021
DOI
https://doi.org/10.1007/978-3-030-52429-6_27

Premium Partners