Year: 1948
Type: report
Abstract: Note presenting the effect on lateral oscillatory stability of varying the value of the stability derivative over a wide range of negative and positive values as determined theoretically for a sweptback fighter airplane with loading conditions simulating an airplane with and without wing-tip fuel tanks.
Authors: Johnson, Joseph L., Sternfield, Leonard
Institution: Langley Memorial Aeronautical Laboratory
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green
OpenAlex ID: W7139444183