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Flight investigation to improve the dynamic longitudinal stability and control-feel characteristics of the p-63a-1 airplane (aaf no. 42-68889) with closely balanced experimental elevators
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1946 |
| Description | Results of flight tests of a control-feel aid presented. This device consisted of a spring and dashpot connected in series between the control stick and airplane structure. The device was tested in combination with an experimental elevator and bobweight which had given unsatisfactory dynamic stability and control-feel characteristics in previous tests. The control-feel aid effected marked improvement in both the control-feel characteristics and the control-feel dynamic longitudinal stability of the airplane. |
| File Size | 31697199 |
| Page Count | 67 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092636 |
| Archival Resource Key | ark:/13960/t0jt40g76 |
| Language | English |
| Publisher Date | 1946-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airplanes - Bell P-63a-1 Flight Tests (amer ) Center OF Gravity - Position Control Sticks - Forces Bob Weignts Stability & Control, Longitudinal - Bell P-63a-1 Elevators, Balanced - Bell P-63a-1 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 |
