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An Analytical Evaluation of the Effects of an Aerodynamic Modification and of Stability Augmenters on the Pitch Behavior and Probable Pilot Opinion of Two Current Fighter Airplanes

Melvin Sadoff

出版	National Advisory Committee for Aeronautics, 1958
URL	http://books.google.com.hk/books?id=gT32ZwEACAAJ&hl=&source=gbs_api

註釋

The effects of a wing modification and of stability augmentation on the computed longitudinal behavior in the pitch-up region and probable pilot opinion of the pitch-up characteristics of two current fighter airplanes are presented.