ED Decision 2020/011/R
This Appendix contains data that defines the Dryden turbulence and discrete gust model to be used in conducting the tests specified in paragraphs 4(d)(7)(ii), 4(d)(7)(iii), 4(d)(8)(ii), and 4(d)(8)(iii) of Appendix 1 to this ETSO.
Dryden Turbulence Model
where:
SIGMAu, SIGMAv, SIGMAw are the RMS intensities;
TAUu = Lu/VA;
TAUv = Lv/VA;
TAUw = Lw/VA;
Lu, Lv, Lw are the turbulence scale lengths; VA is the aircraft’s true airspeed (ft/sec);
PI = 3.1415926535;
PI2 = 6.2831853070 (2 times PI);
SQRT3 = 1.732050808 (square root of 3); and
S is the Laplace transform variable.
The following table lists SIGMAu, SIGMAv, SIGMAw, Lu, Lv, and Lw versus altitude. Extrapolation will not be used, and simulator altitudes outside the bounds of the turbulence list will use the data at the boundary.
Altitude (feet) |
RMS Intensities (ft/sec) |
Scale Lengths (feet) |
||||
Long |
Lat |
Vert |
Long |
Lat |
Vert |
|
100 |
5.6 |
5.6 |
3.5 |
260 |
260 |
100 |
300 |
5.15 |
5.15 |
3.85 |
540 |
540 |
300 |
700 |
5.0 |
5.0 |
4.3 |
950 |
950 |
700 |
900 |
5.0 |
5.0 |
4.45 |
1123 |
1123 |
900 |
1500 |
4.85 |
4.85 |
4.7 |
1579 |
1579 |
1500 |
The applicant shall demonstrate that the variance of their turbulence implementation is adequate.
Discrete Gust Rejection
Discrete gusts (in the horizontal axis) with ranges of amplitude and frequency (A and OMEGA) of the form [A(1 − cos OMEGAt)] shall be used.
The following table lists the values of A and OMEGA to be used (this simulates an approximate 15-knot gust condition):
A |
OMEGA (rad/sec) |
Approx. Gust Duration (sec) |
7.5 |
2.10 |
3 |
7.5 |
1.26 |
5 |
7.5 |
0.78 |
8 |
7.5 |
0.63 |
10 |
7.5 |
0.52 |
12 |
7.5 |
0.42 |
15 |
7.5 |
0.31 |
20 |
[Amdt ETSO/16]
Appendix 4 to ETSO-C117b defines the Dryden turbulence and discrete gust model for specified tests, including RMS intensities, scale lengths, and gust parameters, with no extrapolation beyond table bounds.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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