|
MULTIMEDIA LIBRARY -
METHODS IN HYDRAULICS
FLUID MECHANICS
Shock waves in supersonic
tunnel
Shock Waves - X15 in 4 x 4 Foot Supersonic
Tunnel.
Courtesy of Dr Marian Muste, IIHR - Hydroscience & Engineering,
University of Iowa.
The
Fluids Laboratory
is an integrated learning environment developed by
IIHR-Hydroscience & Engineering
for the
College of Engineering
of
The
University of Iowa.
Shock Waves - X15 in 4 x 4 Foot Supersonic Tunnel - Photograph
published in Sixty Years of Aeronautical Research 1917-1977 By
David A. Anderton (page 51) - a NASA publication - Picutre taken from
NASA Image
eXchange |
