Sign Up to like & get
recommendations!
0
Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.02.015
Abstract: Abstract An innovative type of pressure distribution for the hypersonic aircraft forebody (bump) is presented, and this design is based on the newly established known as pressure ridge (PR) flow mechanism. Studies on the low-kinetic-energy…
read more here.
Keywords:
bump;
pressure ridge;
controllable bump;
pressure controllable ... See more keywords