The effects of flight on noise from heated jets are discussed. The effects of the additionally, extraneously-generated dipole and simple source terms which arise as a result of the density gradients across the fluid interfaces were incorporated. The coaxial flows with inverted profiles are shown to be quieter than the conventional profiles; however, the benefit of noise reduction at higher outer-to-inner area ratios is totally offset as the inverted profile incurs a significant massloss and thrust-loss. Amongst all the possible coaxial configurations when on of the coaxial streams is heated-conventional profile (CP), inverted profile (IP) and the variable stream control engine (VSCE) cycle-and at constant massflow and thrust, a VSCE-cycle i...
Analytical studies based on a turbulent mixing noise prediction technique indicate that jet noise po...
An experimental study is presented of the pressure fluctuations near jet exhaust streams made during...
The presentation highlights jet-noise research conducted in the Subsonic Fixed Wing, Supersonics, an...
The research performed began during Spring 1991 as a project to assess the noise reduction potential...
Relationships between the noise generation characteristics and the flow field characteristics for in...
A basic understanding of the noise reduction mechanisms in shock-free inverted-velocity-profile coan...
Predictions are made for the noise radiation from supersonic, coaxial jets. These predictions are ba...
Jet noise and flow field were measured to follow up on observations made by Professor D. Papamoschou...
Far field noise generation from interacting coaxial jet flows, and nozzle operational mode
The noise from perfectly expanded coaxial jets was measured in an anechoic chamber for different ope...
Experimental results are presented for static acoustic model tests of various geometrical configurat...
Acoustic measurements were made in the 'near' (r/D 60, x/D 60) field for high Reynolds number (184...
In this paper predictions are made for the noise radiation from supersonic coaxial jets. The noise i...
Far-field noise radiated from coaxial cold underexpanded jet flows issuing from convergent two-nozz...
A semi-empirical model for predicting the noise generated by jets exhausting from circular nozzles i...
Analytical studies based on a turbulent mixing noise prediction technique indicate that jet noise po...
An experimental study is presented of the pressure fluctuations near jet exhaust streams made during...
The presentation highlights jet-noise research conducted in the Subsonic Fixed Wing, Supersonics, an...
The research performed began during Spring 1991 as a project to assess the noise reduction potential...
Relationships between the noise generation characteristics and the flow field characteristics for in...
A basic understanding of the noise reduction mechanisms in shock-free inverted-velocity-profile coan...
Predictions are made for the noise radiation from supersonic, coaxial jets. These predictions are ba...
Jet noise and flow field were measured to follow up on observations made by Professor D. Papamoschou...
Far field noise generation from interacting coaxial jet flows, and nozzle operational mode
The noise from perfectly expanded coaxial jets was measured in an anechoic chamber for different ope...
Experimental results are presented for static acoustic model tests of various geometrical configurat...
Acoustic measurements were made in the 'near' (r/D 60, x/D 60) field for high Reynolds number (184...
In this paper predictions are made for the noise radiation from supersonic coaxial jets. The noise i...
Far-field noise radiated from coaxial cold underexpanded jet flows issuing from convergent two-nozz...
A semi-empirical model for predicting the noise generated by jets exhausting from circular nozzles i...
Analytical studies based on a turbulent mixing noise prediction technique indicate that jet noise po...
An experimental study is presented of the pressure fluctuations near jet exhaust streams made during...
The presentation highlights jet-noise research conducted in the Subsonic Fixed Wing, Supersonics, an...