| contributor author | M. Hubbard | |
| contributor author | H. J. Rust | |
| date accessioned | 2017-05-08T23:17:07Z | |
| date available | 2017-05-08T23:17:07Z | |
| date copyright | June, 1984 | |
| date issued | 1984 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26236#406_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/98050 | |
| description abstract | Optimal release conditions for the javelin are studied using computer simulation. Included are two important and realistic assumptions: (1) initial velocity attainable by the thrower is dependent on the throwing angle, and (2) the aerodynamic center of pressure moves as a function of angle of attack. Aerodynamic forces and moments, previously measured in wind tunnel tests, are incorporated in the simulation. Range contours are presented in the two-space of initial angle of attack–initial flight path angle, assuming zero initial angular velocity. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Javelin Dynamics With Measured Lift, Drag, and Pitching Moment | |
| type | Journal Paper | |
| journal volume | 51 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3167632 | |
| journal fristpage | 406 | |
| journal lastpage | 408 | |
| identifier eissn | 1528-9036 | |
| keywords | Dynamics (Mechanics) | |
| keywords | Drag (Fluid dynamics) | |
| keywords | Simulation | |
| keywords | Wind tunnels | |
| keywords | Flight | |
| keywords | Pressure | |
| keywords | Aerodynamics AND Computer simulation | |
| tree | Journal of Applied Mechanics:;1984:;volume( 051 ):;issue: 002 | |
| contenttype | Fulltext | |