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Presentation of the acoustic and aerodynamic results of the aladin 2 concept qualification testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Collard, M. Doyotte, C. Sagner, M. |
| Copyright Year | 1985 |
| Description | Wind tunnel tests were conducted of a scale model of the Aladin 2 aircraft. The propulsion system configuration is described and the air flow caused by jet ejection is analyzed. Three dimensional flow studies in the vicinity of the engine installation were made. Diagrams of the leading and trailing edge flaps are provided. Graphs are developed to show the aerodynamic performance under conditions of various airspeed and flap deflection. |
| File Size | 2452563 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850026848 |
| Archival Resource Key | ark:/13960/t3vt6j08d |
| Language | English |
| Publisher Date | 1985-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aladin 2 Aircraft Air Flow Aerodynamic Configurations Leading Edge Slats Wind Tunnel Tests Flow Visualization Short Takeoff Aircraft Trailing Edge Flaps Propulsion System Configurations Lift Augmentation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |