درباره ما
NACA-TN-703
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics I - four N.A.C.A. 23012 wings of various plan forms with and without dihedral
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:09:32Z | |
| date available | 2017-09-04T16:09:32Z | |
| date copyright | 01/01/1939 | |
| date issued | 1939 | |
| identifier other | SGYIYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/72740 | |
| description abstract | Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tunnel. All the wings have rounded tips and, in plan form, one is rectangular and the others are tapered 3:1 with various amounts of sweep. Each wing was tested with two amounts of dihedral and with partial-span split flaps. The coefficients of lift, drag, and pitching moment are given for all the models at zero yaw. The coefficients of rolling moment, yawing moment, and side force are given for the rectangular wing at all values of yaw tested. The rate of change in the coefficients with angle of yaw is given in convenient form for stability calculations. | |
| language | English | |
| title | NACA-TN-703 | num |
| title | Wind-tunnel investigation of effect of yaw on lateral-stability characteristics I - four N.A.C.A. 23012 wings of various plan forms with and without dihedral | en |
| type | standard | |
| page | 18 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1939 | |
| contenttype | fulltext |
