Theoretical Analysis and Experimental Researches regarding the Asymmetrical Fluid Flow Applied in Aeronautics

Table 1

Nr.crt	Static pressure [N/m^2]	[m/s]	Force [N]	[Nm]	[Nm]
1	101237,4642	4,122222	2,26655	0,063376	−0,010004
2	101239,1528	4,178888	2,31825	0,068185	−0,012168
3	101240,7134	4,210001	2,40756	0,072684	−0,014505
4	101242,4722	4,290344	2,51815	0,076828	−0,01653
5	101244,1634	4,340777	2,62753	0,080975	−0,01827
6	101245,9927	4,386788	2,70147	0,085902	−0,018457
7	101248,1247	4,433453	2,74428	0,093680	−0,018168
8	101250,1457	4,532223	2,77195	0,102288	−0,017179
9	101252,0222	4,544555	2,80014	0,110612	−0,015722
10	101253,6918	4,666677	2,83484	0,116111	−0,013897

: the speed of the fluid through the tail boom.
: lateral force resulted from the Coandă effect.
: torque on direction , -torque on direction .