Local Flow Measurements at the Inlet Spike Tip of a mach 3 Supersonic Cruise Airplane PDF
42 Pages·2001·1.54 MB·English
Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.
Preview Local Flow Measurements at the Inlet Spike Tip of a mach 3 Supersonic Cruise Airplane
Description:
stream Mach numbers from 1. 6 to 3. 0. Local flow angularity, Mach number, free—stream Mach numbers, angle of attack, and angle of sideslip.
See more
The list of books you might like
Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.
