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Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-meter diameter single rotor
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mineck, R. E. Freeman, C. E. |
| Copyright Year | 1979 |
| Description | A wind-tunnel investigation was conducted to measure the time averaged fuselage surface pressures of a helicopter model with a 3.15 meter diameter, four-bladed articulated rotor. Measurements were made at hover and advance ratios of 0.05, 0.15, and 0.20 for a range of thrusts. Data are presented with no analysis. |
| File Size | 4584685 |
| Page Count | 170 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790017844 |
| Archival Resource Key | ark:/13960/t81k46s7v |
| Language | English |
| Publisher Date | 1979-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wind Tunnel Tests Wind Tunnel Models Fuselages Pressure Measurement Helicopters Rotary Wings Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |