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Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Batterson, J. G. Suit, W. T. |
| Copyright Year | 1986 |
| Description | The aerodynamics of the basic F-106B were determined at selected points in the flight envelope. The test aircraft and flight procedures were presented. Aircraft instrumentation and the data system were discussed. The parameter extraction procedure was presented along with a discussion of the test flight results. The results were used to predict the aircraft motions for maneuvers that were not used to determine the vehicle aerodynamics. The control inputs used to maneuver the aircraft to get data for the determination of the aerodynamic parameters were discussed in the flight test procedures. The results from the current flight tests were compared with the results from wind tunnel test of the basic F-106B. |
| File Size | 1245522 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860015232 |
| Archival Resource Key | ark:/13960/t0qr9pz42 |
| Language | English |
| Publisher Date | 1986-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Flight Stability Tests Data Processing F-106 Aircraft Regression Analysis Parameter Identification Flight Envelopes Wind Tunnel Tests Aircraft Maneuvers Mathematical Models Maximum Likelihood Estimates Aerodynamic Characteristics Flight Simulation Mach Number 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 |
