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Experimental verification of low sonic boom configuration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ferri, A. Sorensen, H. Wang, H. H. |
| Copyright Year | 1972 |
| Description | A configuration designed to produce near field signature has been tested at M = 2.71 and the results are analyzed, by taking in account three-dimensional and second order effects. The configuration has an equivalent total area distribution that corresponds to an airplane flying at 60,000 ft. having a weight of 460,000 lbs, and 300 ft. length. A maximum overpressure of 0.95 lb/square foot has been obtained experimentally. The experimental results agree well with the analysis. The investigation indicates that the three-dimensional effects are very important when the measurements in wind tunnels are taken at small distances from the airplane. |
| File Size | 2465404 |
| Page Count | 113 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720022357 |
| Archival Resource Key | ark:/13960/t4tj38n0t |
| Language | English |
| Publisher Date | 1972-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Shock Waves Numerical Analysis Aerodynamic Configurations Supersonic Flight Aircraft Design Sonic Booms Wind Tunnel Models Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
