↓ Skip to main content
Altmetric
What is this page?
Embed badge
Share
Share on Twitter
Share on Facebook
Share by email
Shock tunnel study of spiked aerodynamic bodies flying at hypersonic Mach numbers
Overview of attention for article published in Shock Waves, November 2002
Altmetric Badge
About this Attention Score
Among the highest-scoring outputs from this source (#22 of 317)
Mentioned by
patent
1
patent
Citations
dimensions_citation
51
Dimensions
Readers on
mendeley
26
Mendeley
Summary
Patents
Dimensions citations
So far, Altmetric has seen
1
patent that references this research output.
Device for influencing a supersonic - flow around
Grant DE-102009001953-B4
Germany
14 Nov 2013