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High-attitude low-speed static aerodynamic characteristics of an f-4d fighter airplane model with leading edge slats
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Monfort, J. C. Whitcomb, W. M. |
| Copyright Year | 1975 |
| Description | An investigation was conducted to determine the effects of two-position leading edge slats on the low speed aerodynamic characteristics of a swept wing twin-jet supersonic fighter airplane model at high angle of attack and various Reynolds numbers. The investigation was performed at a Mach number of 0.20 over a range of angle of attack from 19 deg to 90 deg and angles of slideslip from -10 deg to 30 deg and Reynolds numbers from 1.97 to 13.12 million per meter. |
| File Size | 6400996 |
| Page Count | 183 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760019102 |
| Archival Resource Key | ark:/13960/t8x97086m |
| Language | English |
| Publisher Date | 1975-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Low Speed Stability High Altitude Riding Quality Swept Wings Leading Edge Slats F-4 Aircraft Angle of Attack Aerodynamic Characteristics Aerodynamic Stalling Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
