The zero-lift drag of a 60 degree delta-wing-body combination (AGARD model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7

Author: Piland, Robert O
Year: 1954
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3081
Link: https://digital.library.unt.edu/ark:/67531/metadc56898/

< New search