Continuous gusts
Continuous gusts or stochastic gusts are winds that vary randomly in space and time. Models of continuous gusts are used to represent
Models of continuous gusts
A variety of models exist for gusts
Assumptions of continuous gust models
The models accepted by the FAA and Department of Defense represent continuous gusts as a wind linear and angular velocity field that is a random process and make a number of simplifying assumptions in order to describe them mathematically. In particular, continuous gusts are assumed to be:[8]
- A Gaussian process
- A stationary process, so the statistics are constant in time
- Homogeneous, so the statistics do not depend on the vehicle path
- Ergodic
- Isotropic at high altitude, so the statistics do not depend on the vehicle attitude
- Varying in space but frozen in time
These assumptions, while unrealistic, yield acceptable models for flight dynamics applications.[9] The last assumption of a velocity field that does not vary with time is especially unrealistic, since measurements of atmospheric turbulence at one point in space always vary with time. These models rely on the airplane's motion through the gusts to generate temporal variations in wind velocity, making them inappropriate for use as inputs to models of hovering, wind turbines, or other applications that are fixed in space.
The models also make assumptions about how continuous gusts vary with altitude. The Dryden and von Kármán models specified by the Department of Defense define three different altitude ranges: low, 10 ft to 1000 ft
Dryden model
The Dryden model is one of the most commonly used models of continuous gusts. It was first published in 1952.[12] The power spectral density of the longitudinal linear velocity component is
where ug is the gusts' longitudinal linear velocity component, σu is the turbulence intensity, Lu is the turbulence scale length, and Ω is a spatial frequency.[2]
The Dryden model has rational power spectral densities for each velocity component. This means that an exact filter can be formed that takes white noise as an input and outputs a random process with the Dryden model's power spectral densities.[6]
von Kármán model
The von Kármán model is the preferred model of continuous gusts for the Department of Defense and the FAA.[1][2] The model first appeared in a 1957 NACA report[13] based on earlier work by Theodore von Kármán.[14][15][16] In this model, the power spectral density of the longitudinal linear velocity component is
where ug is the longitudinal linear velocity component, σu is the turbulence intensity, Lu is the turbulence scale length, and Ω is a spatial frequency.[2]
The von Kármán model has irrational power spectral densities. So, a filter with a white noise input that outputs a random process with the von Kármán model's power spectral densities can only be approximated.[7]
Altitude dependence
Both the Dryden and von Kármán models are parameterized by a length scale and turbulence intensity. The combination of these two parameters determine the shape of the power spectral densities and therefore the quality of the models' fit to spectra of observed turbulence. Many combinations of length scale and turbulence intensity give realistic power spectral densities in the desired frequency ranges.[4] The Department of Defense specifications include choices for both parameters, including their dependence on altitude, which are summarized below.[10]
Low altitude
Low altitude is defined as altitudes between 10 ft AGL and 1000 ft AGL.
Length scales
At low altitude, the scale lengths are functions of altitude,
where h is the altitude AGL. At 1000 ft AGL, Lu = 2Lv = 2Lw = 1000 ft.
Turbulence intensities
At low altitude, the turbulence intensities are parameterized by W20, the wind speed at 20 ft.
Turbulence severity | |
---|---|
Light | 15 kts |
Moderate | 30 kts |
Severe | 45 kts |
At 1000 ft AGL,
Medium/high altitude
Medium/high altitude is defined as 2000 ft AGL and above.
Length scales
For the Dryden model,
For the von Kármán model,
Turbulence intensities
At high altitude,
They are parameterized by the
Between low and medium/high altitude
From 1000 ft AGL to 2000 ft AGL, both the length scale and turbulence intensity are determined by linear interpolation between the low altitude value at 1000 ft and the medium/high altitude value at 2000 ft.[6][7]
Turbulence axes
Above 1750 ft, the axes of the turbulence coincide with the
See also
- Clear air turbulence
- Dryden Wind Turbulence Model
- Von Kármán wind turbulence model
Notes
- ^ a b 14 CFR Part 25: Appendix G (2011). "Airworthiness Standards: Transport Category Airplanes". U.S. Code of Federal Regulations. Government Printing Office.
{{cite web}}
: CS1 maint: numeric names: authors list (link) - ^ a b c d e MIL-STD-1797A 1990, p. 678.
- ^ MIL-STD-1797A 1990, pp. 695–697.
- ^ a b Hoblit 1988, Chap. 4.
- ^ Etkin 2005, pp. 543–562.
- ^ a b c "Dryden Wind Turbulence Model (Continuous)". MATLAB Reference Pages. The MathWorks, Inc. 2010. Retrieved May 24, 2013.
- ^ a b c "Von Karman Wind Turbulence Model (Continuous)". MATLAB Reference Pages. The MathWorks, Inc. 2010. Retrieved May 24, 2013.
- ^ Etkin 2005, pp. 531–543.
- ^ Hoblit 1988, Chap. 12.
- ^ a b MIL-STD-1797A 1990, pp. 673, 678–685, 702.
- ^ MIL-STD-1797A 1990, p. 680.
- doi:10.2514/8.2491.
- ^ Diedrich, Franklin W.; Joseph A. Drischler (1957). Effect of Spanwise Variations in Gust Intensity on the Lift Due to Atmospheric Turbulence (Report). pp. NACA TN 3920.
- .
- PMID 16588830.
- ISBN 9780080563800.
- ^ MIL-STD-1797A 1990, p. 673.
- ^ MIL-STD-1797A 1990, p. 702.
References
- Etkin, Bernard (2005). Dynamics of Atmospheric Flight. Mineola, NY: Dover Publications. ISBN 0486445224.
- Hoblit, Frederic M. (1988). Gust Loads on Aircraft: Concepts and Applications. Washington, DC: American institute of Aeronautics and Astronautics, Inc. ISBN 0930403452.
- Flying Qualities of Piloted Aircraft (PDF). Vol. MIL-STD-1797A. United States Department of Defense. 1990.