left-click = rotate, middle-button/CTLR-left-click = pan, scroll/right-click/ALT-left-click = zoom
|Description||This version of the Cessna 210 is based on the NASA study into the efficacy of high percentage laminar flow wings. Information on the study and the corresponding drag buildup files can be found on the wiki at: http://www.openvsp.org/wiki/doku.php?id=dragverification|
3 - The source material used to create this model was Good. This means good 3-view drawings were used to create the model.