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NOTES CONCERNING THE TRANSITION EXPERIMENT

1st AIAA CFD High Lift Prediction Workshop


image of trap wing model in 14x22

 

In the process of conducting the transition experiments on the Trap Wing model (Configuration 1) in the NASA Langley 14x22 Wind Tunnel, the lead experimentalists assembled notes concerning the process which led to the information provided in the published report AIAA-2005-5148 (McGinley et al, June 2005). As an aid to the CFD community interested in making use of the experimental information given in this AIAA paper, some of these notes are provided here.

DISCLAIMER: The information contained in this and following sections constitutes a set of informal notes only and is not necessarily complete. Use with caution. For further details, see the published AIAA paper listed above.


 

Overall Summary (click on each image to view it larger):
transition summary, upper surface 12 deg transition summary, lower surface 12 deg
transition summary, upper surface 16 deg transition summary, lower surface 16 deg
transition summary, upper surface 24 deg transition summary, lower surface 24 deg

In the following tables, clicking on an object number brings up typical hot-film time-signal plots for that object (if available).

Upper surface Alpha=12.96 deg (corrected):
1
2
3
4
5
6
7
8
19
20
21
22
23
24
25
26
27
28
37
40

Notes: Objects 1 & 2 are turbulent; Object 3 is a strip and shows the end of transition to turbulence with the skewness flipping at film 1.

Lower surface Alpha=12.96 deg (corrected):
9
10
11
12
13
14
15
16
17
18
29
30
31
32
33
34
35
36
38
39

Upper surface Alpha=17.10 deg (corrected):
1
2
3
4
5
6
7
8
19
20
21
22
23
24
25
26
27
28
37
40

Lower surface Alpha=17.10 deg (corrected):
9
10
11
12
13
14
15
16
17
18
29
30
31
32
33
34
35
36
38
39

Upper surface Alpha=25.33 deg (corrected):
1
2
3
4
5
6
7
8
19
20
21
22
23
24
25
26
27
28
37
40

Notes: Objects 1, 2, and 20 are turbulent.

Lower surface Alpha=25.33 deg (corrected):
9
10
11
12
13
14
15
16
17
18
29
30
31
32
33
34
35
36
38
39


 

The following links provide some informal experimentalist's notes regarding transition over each of the three Trap Wing elements:


 

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Page Curator and NASA Official Responsible for Content
Christopher Rumsey  

Last Updated
September 16, 2011

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