| dc.contributor.advisor | Rao, Balusu M. | |
| dc.creator | Cogan, Thomas Joseph | |
| dc.date.accessioned | 2022-04-01T16:02:00Z | |
| dc.date.available | 2022-04-01T16:02:00Z | |
| dc.date.issued | 1977 | |
| dc.identifier.uri | https://hdl.handle.net/1969.1/CAPSTONE-ProppeD_1998 | |
| dc.description | Program year: 1976/1977 | en |
| dc.description | Digitized from print original stored in HDR | en |
| dc.description.abstract | A recent development of the NASA Airfoil Research Program is a family of new high lift, low drag airfoils for application on general aviation aircraft. This study analyzes one of these airfoils, the 13% thick GA(W)-2, as to its lift, drag, and pitching moment characteristics, and compares it to airfoils used on current production aircraft. The analysis includes the results of two-dimensional wind tunnel tests as well as theoretical calculations made using thin airfoil theory and a lifting surface method. | en |
| dc.format.extent | 42 pages | en |
| dc.format.medium | electronic | en |
| dc.format.mimetype | application/pdf | |
| dc.subject | NASA Airfoil Research Program | en |
| dc.subject | general aviation aircraft | en |
| dc.subject | airfoils | en |
| dc.subject | thin airfoil theory | en |
| dc.subject | lifting surface method | en |
| dc.title | Low Speed Areodynamic Analysis Of The Nasa GA(W)-2 Airfoil | en |
| dc.title.alternative | LOW SPEED AREODYNAMIC ANALYSIS OF THE NASA GA(W)-2 AIRFOIL | en |
| dc.type | Thesis | en |
| thesis.degree.department | Aerospace Engineering | en |
| thesis.degree.grantor | University Undergraduate Fellow | en |
| thesis.degree.level | Undergraduate | en |
| dc.type.material | text | en |
