CFD Analysis of Nozzle Jet Plume Effects on Sonic Boom Signature

By: Administration (Nasa), National Aeronaut

Technical Report Bui, Trong T. Armstrong Flight Research Center NASA/TM-2009-214650, AIAA Paper 2009-1054, H-2923, DFRC-938 COMPUTATIONAL FLUID DYNAMICS; NOZZLE FLOW; GAS JETS; NOZZLE GEOMETRY; SONIC BOOMS; WIND TUNNEL TESTS; PLUMES; F-15 AIRCRAFT; SUPERSONIC AIRCRAFT; VISCOSITY; RESEARCH AIRCRAFT; SIGNATURES; COMPUTATIONAL GRIDS

• Format: Paperback
• Language: English
• ISBN: B08F6Y3SNM
• ISBN13: 9798673044995
• Release Date: January 1
• Publisher: Independently Published
• Length: 48 Pages
• Weight: 0.30 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"