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Low-speed aerodynamic characteristics of a fuselage model with various arrangements of elongated lift jets
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Goodson, K. W. Vogler, R. D. |
| Copyright Year | 1973 |
| Description | Data were obtained for a round jet located on the center of the bottom of a fuselage and for elongated slots separated spanwise by distances of 0.8 and 1.2 of the fuselage width. The effect of yawing the slots, inclining the jets laterally, and combining slot yaw with jet inclination was determined. Data were obtained in and out of ground effect through a range of effective velocity ratios and through a range of sideslip angles. |
| File Size | 7254645 |
| Page Count | 86 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730022207 |
| Archival Resource Key | ark:/13960/t91882m27 |
| Language | English |
| Publisher Date | 1973-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft V/stol Aircraft Nozzle Flow Jet Flow Jet Nozzles Ground Effect Aerodynamics Aerodynamic Characteristics Lift Augmentation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |