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Language: en
Pages: 48
Pages: 48
Type: BOOK - Published: 2019-01-14 - Publisher: Independently Published
A computational fluid dynamics study is conducted to examine nozzle exhaust jet plume effects on the Sonic boom signature of a supersonic aircraft. A simplified
Language: en
Pages: 50
Pages: 50
Type: BOOK - Published: 2013-07 - Publisher: BiblioGov
A computational fluid dynamics study is conducted to examine nozzle exhaust jet plume effects on the Sonic boom signature of a supersonic aircraft. A simplified
Language: en
Pages: 40
Pages: 40
Type: BOOK - Published: 2009 - Publisher:
A computational fluid dynamics study is conducted to examine nozzle exhaust jet plume effects on the sonic boom signature of a supersonic aircraft. A simplified
Language: en
Pages: 28
Pages: 28
Type: BOOK - Published: 2013-07 - Publisher: BiblioGov
Reducing or eliminating the operational restrictions of supersonic aircraft over populated areas has led to extensive research at NASA. Restrictions were due to
Language: en
Pages: 26
Pages: 26
Type: BOOK - Published: 2018-05-22 - Publisher: Createspace Independent Publishing Platform
Fundamental research for sonic boom reduction is needed to quantify the interaction of shock waves generated from the aircraft wing or tail surfaces with the ex