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Pressure measurements on the leading edge of a swept wing at mach 2.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sorrells II, R. B. |
| Copyright Year | 1974 |
| Description | Detailed pressure measurements were made on a flat semispan swept wing with a rounded leading edge at Mach number 2.2 through a range of Reynolds numbers. Pressure orifices were distributed in the streamwise direction at five spanwise stations on the leading edge and on the upper and lower surfaces. No significant amount of leading-edge suction was found, but the pressures and integrated normal forces on the upper and lower surfaces indicate the presence of a vortex lift. |
| File Size | 10514951 |
| Page Count | 109 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019367 |
| Archival Resource Key | ark:/13960/t94795c9p |
| Language | English |
| Publisher Date | 1974-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Configurations Swept Wings Supersonic Speed Pressure Distribution Aerodynamic Coefficients Pressure Measurement Leading Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
