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Comparison of wind tunnel and flyover noise measurements of the yov-10a stol aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Atencio Jr., A. Soderman, P. T. |
| Copyright Year | 1972 |
| Description | The YOV-10A Research Aircraft was flown to obtain flyover noise data that could be compared to noise data measured in the 40- by 80- foot wind tunnel at NASA Ames Research Center. The flyover noise measurements were made during the early morning hours on runway 32L at Moffett Field, California. A number of passes were made at 50 ft altitude in level flight with an airplane configuration closely matching that tested in the wind tunnel. Two passes were selected as prime and were designated for full data reduction. The YOV-10A was flown over a microphone field geometrically similar to the microphone array set up in the wind tunnel. An acoustic center was chosen as a matching point for the data. Data from the wind tunnel and flyover were reduced and appropiate corrections were applied to compare the data. Results show that wind tunnel and flight test acoustic data agreed closely. |
| File Size | 1364613 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720019381 |
| Archival Resource Key | ark:/13960/t4cp1w10s |
| Language | English |
| Publisher Date | 1972-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Noise Propagation Acoustic Measurement Aircraft Noise Short Takeoff Aircraft Ov-10 Aircraft Noise Spectra Sound Pressure Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |