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Tests on an airplane model, AEG D I of the Allgemeine Elektricitats Gesellschft, A-G, airplane construction section conducted at the Gottingen Model Testing Laboratory for Aerodynamics (1923) NASA Technical Reports Server (NTRS) · leaf 25
- S5 - Table 4 (Cont.) . Experiments ^ith Variations in the Elevator Adjustment and also without Tail Group* Stabilizer 6^ 30'. Aileron 0 Elevator 20° Rudder 0 … -2.1 . 185 0. 2 . 227 1.7 . 336 3.3 . 351 4. 5 , 257 5. 5 . 270 6.1 . 283 6. 4 . 293 6-6 . 304' 6. 5 . 312 6. 8 . 334 4.9 . 374 Aileron 0 -1.9 . 232 0. 4 . 367 1.7 , 273 3.3 . 290 4. 3 . 301 5. 3 . 315 5. 8 . 316 6. 3 ..331 6. 3 . 333 6. 3 . 336 5.7 . 348 4. 6 . 384 NASA Technical Reports Server (NTRS)
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