Most of the aerodynamic configurations considered are suitable for highly maneuverable air-to-air or surface-to-air missiles; however, data for a few air-to-surface, cruise missiles, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range.
Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis
1977
126 pages
Report
Keine Angabe
Englisch