WorldCat Identities

Neuwerth, G.

Overview
Works: 10 works in 11 publications in 2 languages and 12 library holdings
Roles: Author
Publication Timeline
.
Most widely held works by G Neuwerth
Lärmminderungsmaßnahmen bei kolbengetriebenen Flugzeugen der Allgemeinen Luftfahrt : Schlußbericht ; Förderzeitraum: 15.7.1996-31.10.1999 by R Drobietz( )

2 editions published between 1999 and 2000 in German and held by 3 WorldCat member libraries worldwide

Aircraft noise, Muffler, exhaust noise, ceramics, propeller noise, sweep
Analyse Gezielter Massnahmen zur Reduzierung des Laerms von Mantelschrauben Abschlussbericht by R Staufenbiel( Book )

1 edition published in 1980 in German and held by 1 WorldCat member library worldwide

Anhang zur Steuerungsanalyse( Book )

1 edition published in 1980 in German and held by 1 WorldCat member library worldwide

Akustische Reuckkopplungserscheinungen am Unter- und eUberschallfreistrahl, der auf einen Steorkeorper trifft by G Neuwerth( Book )

1 edition published in 1972 in German and held by 1 WorldCat member library worldwide

Theorie der Ausbreitung wellenfeormiger Steorungen entgegen Streomungsrichtung in einem Unterschall-Freistrahl by G Neuwerth( Book )

1 edition published in 1974 in German and held by 1 WorldCat member library worldwide

Moduloptimierung und Steuerungsanalyse( Book )

1 edition published in 1980 in German and held by 1 WorldCat member library worldwide

Bordgebundenes Verfahren zur Messung von Scherwindgradienten : Jahrestagung der DGLR, Aachen, den 12. bis 14. Mai 1981 by G Neuwerth( Book )

1 edition published in 1981 in German and held by 1 WorldCat member library worldwide

Theory for the Propagation of Undulating Disturbances Upstream in a Subsonic Free Jet( Book )

1 edition published in 1975 in English and held by 1 WorldCat member library worldwide

Experimental observations have shown that a periodic pressure disturbance inside a subsonic jet propagates upstream in a way that may be explained as waves traveling obliquely to a jet axis, which are totally reflected at the jet boundary layer. This pressure wave induces axisymmetric ring vortices in the free boundary near the nozzle exit, which intensifies the noise of the jet considerably. A good agreement between the solutions for a clear model representation and the results of the theoretical computation of the propagation of undulating disturbances traveling upstream is found. Outside the jet a near field is induced, and its decrease perpendicular to the jet is computed
Akustische Rückkopplungserscheinungen beim Düsenlärm by G Neuwerth( Book )

1 edition published in 1972 in German and held by 1 WorldCat member library worldwide

 
Audience Level
0
Audience Level
1
  Kids General Special  
Audience level: 0.90 (from 0.78 for Theory for ... to 0.99 for Theory for ...)

Languages