ARC-E-DAA-TN28746 · Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flows with Shock Interactions
NASA (NTRS) · 2016
Overview
NASA and the U.S. aerospace industry are performing studies of supersonic aircraft concepts with low sonic boom pressure signatures. The computational analyses of modern aircraft designs have matured to the point where there is confidence in the prediction of the pressure signature from the front…
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
Permanent URL — we don’t break links.
Document details
- Doc number ·
- ARC-E-DAA-TN28746
- Publisher ·
- NASA (NTRS)
- Year ·
- 2016
- File size ·
- 13 MB