Unsteady Barebody Cf Data:

Each file in table1 gives unsteady, barebody, skin-friction data at a specific instantaneous angle of attack. In each file, there are 14 pairs of columns. Each pair represents the data at a specific x/L location (L is the model length). First column of each pair is the circumferential location phi , and the second column is the skin friction value. The x/L locations are (in order) : 0.110, 0.131, 0.170, 0.266, 0.306, 0.345, 0.434, 0.501,0.570, 0.638, 0.706, 0.774, 0.819,  and 0.863. Instantaneous angle of attack, and the corresponding non-dimensional time t' of the maneuver is specified in the first column of table 1 for each unsteady file.

Table 1: Unsteady, barebody, skin-friction data at a specific instantaneous angle of attack

File
      figure number in chapter 6 of ref. [1]
unsteady, barebody, t'=3.417, a (t') = 3.1°
figure 6.1
 unsteady, barebody, t'=3.818, a (t') = 5.1°
figure 6.2
unsteady, barebody, t'=4.238, a (t') = 7.2°
figure 6.3
unsteady, barebody, t'=4.696, a (t') = 9.3°
 figure 6.4
unsteady, barebody, t'=5.307, a (t') = 11.3°
 figure 6.5
unsteady, barebody, t'=5.785, a (t') = 13.2°
figure 6.6
unsteady, barebody, t'=6.128, a (t') = 15.3°
figure 6.7
unsteady, barebody, t'=6.472, a (t') = 17.4°
figure 6.8
unsteady, barebody, t'=6.815, a (t') = 19.4°
figure 6.9
unsteady, barebody, t'=7.235, a (t') = 21.4°
figure 6.10
unsteady, barebody, t'=7.655, a (t') = 23.4°
figure 6.11
unsteady, barebody, t'=8.175, a (t') = 25.5°
figure 6.12
unsteady, barebody, t'=10.290, a (t') = 27.6°
figure 6.13