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Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method
| Content Provider | HathiTrust Digital Library |
|---|---|
| Author | Sleeman, William C Becht, Robert E |
| Editor | Robert E. Becht William C. Sleeman |
| Organization | United States. National Advisory Committee for Aeronautics. |
| Description | This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included |
| Volume Number | L9G22A |
| Language | English |
| Publisher | National Advisory Committee for Aeronautics |
| Publisher Date | 1949-01-01 |
| Publisher Place | Washington D.C. |
| Access Restriction | Open |
| Rights License | Items in this record are available as Public Domain, Google-digitized. View the access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements |
| Subject Keyword | Wind tunnel testing Charts, diagrams, etc Pitching (Aerodynamics) Drag (Aerodynamics) Lift (Aerodynamics) Aerofoils Airplanes |
| Content Type | Text |
| Resource Type | Book |
