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Longitudinal aerodynamic characteristics of 45 deg swept wings at mach approximately 0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lamar, J. E. |
| Copyright Year | 1976 |
| Description | Wind tunnel tests were conducted in the Langley 7 x 10 foot wind tunnel at Mach numbers less than 0.20 and at Reynolds numbers less than 3.74 million. The effect of the aft area on the 45 deg swept wing longitudinal aerodynamic characteristics at low subsonic speeds and at an angle of attack range from approximately -2 deg to 28 deg was studied. The data are presented without analysis. |
| File Size | 3775633 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770007047 |
| Archival Resource Key | ark:/13960/t6935mm72 |
| Language | English |
| Publisher Date | 1976-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Drag Pitching Moments Subsonic Speed Swept Wings Wind Tunnel Tests Angle of Attack Aerodynamic Characteristics Longitudinal Stability Lift Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |