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A Low-Speed Investigation of a Fuselage-Side Air Inlet for Use at Transonic Flight Speeds
| Content Provider | University of North Texas |
|---|---|
| Author | Nichols, Mark R. Goral, Edwin B. |
| Organization | Langley Aeronautical Laboratory |
| Description | Low-speed pressure-recovery and surface-pressure measurements for a twin fuselage-side air-inlet arrangement intended for use at transonic speeds are presented. The model was developed by adding a canopy and nose-wheel fairing to basic transonic annular inlet studied in TN 2685. The results indicate shape requirements of fuselage nose, canopy, and nose-wheel fairing for maintaining substream surface velocities everywhere ahead of entrance. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc57073 |
| Language | English |
| Publisher Date | 2019-01-14 |
| Access Restriction | Open |
| Subject Keyword | aircraft inlets aerodynamics |
| Content Type | Text |
| Resource Type | Report |
