Zero-Lift Drag of the Chance Vought Regulus II Missile at Mach Numbers Between 0.8 and 2.2 as Determined From the Flight Tests of Two 0.12-Scale Models: TED No. NACA AD 398

Author: Church, James D.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL54H02
Link: https://digital.library.unt.edu/ark:/67531/metadc60679/

< New search