Longitudinal Frequency-Response and Stability Characteristics of the Douglas D-558-II Airplane as Determined From Transient Response to a Mach Number of 0.96
| Author: | Holleman, Euclid C. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52E02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59160/ |