An investigation has been made in the Mach number range from 0.50 to 2.86 to determine the longitudinal and lateral aerodynamic characteristics of a cruise missile having a 58 deg swept wing and conventional aft tails. Such a vehicle might be applicable to missions such as surface- or air-launched tactical or strategic missiles, unmanned reconnaissance, or countermeasure decoys. (Author)
Aerodynamic Characteristic of a Swept-Wing Cruise Missile at Mach Numbers from 0.50 to 2.86
1972
44 pages
Report
Keine Angabe
Englisch