This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Devices for Improvement of Controllability at Stall
Annotation ability available
Sector:
Language:
English
Abstract
The stall characteristics of Learjet aircraft are discussed in terms of the aerodynamic phenomena which determine the stall behavior. A number of devices are described which have been flight tested in attempting to improve controllability at stall. Theories are offered to explain the effects of each device. Wind tunnel test data are compared with some of the flight results.
Recommended Content
Technical Paper | Aerodynamic Design Approach to the Stall/Spin Problem - The VariViggen |
Technical Paper | Engineering Solutions for Circulation Control Applications |
Technical Paper | Gulfstream II Aerodynamic Design |
Authors
Citation
Hinson, M., "Devices for Improvement of Controllability at Stall," SAE Technical Paper 830723, 1983, https://doi.org/10.4271/830723.Also In
References
- Shevell R.S. Schaufele, R.D. "Aerodynamic Design Features of the DC-9" Journal of Aircraft 1966 515 523
- Schuringa Tj. "Aerodynamics of Wing Stall of the Fokker F28" AGARD-CP-102, Fluid Dynamics of Aircraft Stalling 1972
- McCullough G.B. Gault Donald E. "Examples of Three Representative Types of Airfoil- Section Stall at Low Speed" NACA TM 2502, September 1951
- Gault, D.E. "A Correlation of Low-Speed Airfoil-Section Stalling Characteristics with Reynolds Number and Airfoil Geometry" NACA TN 3963 1957
- Howe, D.C. "Airfoil Stall Prediction with 2-D Wind Tunnel and 3-D Flight Verification" 1983
- Gaster, M. "The Structure and Behavior of Laminar Separation Bubbles" A.R.C. R.&M. Mo. 3595 1967
- Braslow, A.L. Hicks, R.M. Harris, R.V. Jr "Use of Grit-Type Boundary-Layer- Transition Trips on Wind-Tunnel Models" NASA TN D-3579 1966
- Stevens, W.A. Goradia, S.H. Braden, J.A. "Mathematical Model for Two-Dimensional Multi-Component Airfoils in Viscous Flow" NASA CR-1843 1971