| | NACA UK Mirror report description page (Site not responding. Last check: 2007-10-28) |
 | | The effects of ice formations on the section lift, drag, and pitching-moment coefficients of an unswept NACA 65A004 airfoil section of 6-foot chord were studied. |
 | | In general, icing of the airfoil at angles af attack less than 4 degrees caused large increases in section drag coefficients (as much as 350 percent in 8 minunes of heavy glaze icing), reductions in section lift coefficients (up to 13 percent), and changes in the pitching-moment coefficient from diving toward climbing moments. |
 | | Rotation of the iced airfoil to angles of attack other than that at which icing occurred caused sufficiently large changes in the pitching-moment coefficient that, in flight, rapid corrections in trim might be required in order to avoid a hazardous situation. |
| naca.central.cranfield.ac.uk /report.php?NID=7237 (291 words) |