Flow and Acoustic Characteristics of Complex Supersonic Jets

Flow and Acoustic Characteristics of Complex Supersonic Jets PDF Author: Kalyan Goparaju
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 174

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Book Description
Jet noise has been a major source of concern for commercial and military aviation sectors alike. The need to assuage the adverse impact of jet noise on human health has led to increased interest in jet noise source identification and noise level minimization/mitigation. Most previous works on common round supersonic jets have primarily explored the ideal case of simple, perfectly expanded jet configurations. In real world scenarios however, many of these simplifications do not hold. Two such considerations are examined in this work. The first is a simple configuration operating at complex operating conditions, specifically an imperfect expansion i.e. where the jets are operating at off-design conditions. The second concerns a complex configuration at simple conditions: specifically two jets (twin-jets such as those on fighter aircraft) operating in close proximity to each other. In this work, Large Eddy Simulation (LES) based high-fidelity computations are used to understand the dynamics of imperfectly expanded and twin-jets respectively, with the following objectives: 1) Identify the impact of active flow control techniques on the plume dynamics and acoustic characteristics of underexpanded jets, and 2) Investigate the interaction dynamics of the twin-jet plumes and study its associated sound field which exhibits complex radiation characteristics.

Flow and Acoustic Characteristics of Complex Supersonic Jets

Flow and Acoustic Characteristics of Complex Supersonic Jets PDF Author: Kalyan Goparaju
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 174

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Book Description
Jet noise has been a major source of concern for commercial and military aviation sectors alike. The need to assuage the adverse impact of jet noise on human health has led to increased interest in jet noise source identification and noise level minimization/mitigation. Most previous works on common round supersonic jets have primarily explored the ideal case of simple, perfectly expanded jet configurations. In real world scenarios however, many of these simplifications do not hold. Two such considerations are examined in this work. The first is a simple configuration operating at complex operating conditions, specifically an imperfect expansion i.e. where the jets are operating at off-design conditions. The second concerns a complex configuration at simple conditions: specifically two jets (twin-jets such as those on fighter aircraft) operating in close proximity to each other. In this work, Large Eddy Simulation (LES) based high-fidelity computations are used to understand the dynamics of imperfectly expanded and twin-jets respectively, with the following objectives: 1) Identify the impact of active flow control techniques on the plume dynamics and acoustic characteristics of underexpanded jets, and 2) Investigate the interaction dynamics of the twin-jet plumes and study its associated sound field which exhibits complex radiation characteristics.

Flow and Acoustic Characteristics of Subsonic and Supersonic Jets from Convergent Nozzle

Flow and Acoustic Characteristics of Subsonic and Supersonic Jets from Convergent Nozzle PDF Author: Henry T. Nagamatsu
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90

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Flow and Acoustic Properties of Low Reynolds Number Underexpanded Supersonic Jets

Flow and Acoustic Properties of Low Reynolds Number Underexpanded Supersonic Jets PDF Author: Tieh-Feng Hu
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Measurements on the Flow and Acoustic Properties of a Moderate Reynolds Number Supersonic Jet

Measurements on the Flow and Acoustic Properties of a Moderate Reynolds Number Supersonic Jet PDF Author: Timothy Ray Troutt
Publisher:
ISBN:
Category :
Languages : en
Pages : 194

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Measured Acoustic Characteristics of Ducted Supersonic Jets at Different Model Scales

Measured Acoustic Characteristics of Ducted Supersonic Jets at Different Model Scales PDF Author: R. R. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Supersonic Flow and Its Control Over Highly Three-dimensional Cavities

Supersonic Flow and Its Control Over Highly Three-dimensional Cavities PDF Author: Michael Vincent Sheehan
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description
To accomplish this goal, two additional models were constructed each having only one of the additional geometrical features, either diverging side walls or the ramp floor. Subsequently it was determined that biggest impact on changing the cavity acoustics came from the diverging side walls of the complex cavity. In addition to testing the effect of cavity geometry, a microjet control technique was adapted to reduce the pressure loads within the highly three-dimensional cavity. An array consisting of eight 400micrometer diameter jets was used, and with minimal mass flow, reductions of both the tonal amplitudes and broadband levels was possible. Along with testing on the very small scale, experiments were conducted with the same complex geometry nearly 10 times larger. Two major results were found: first the baseline, no control, acoustics of both the large and small models were found to scale quite well, moreover the microjet control technique was found to be similarly effective one the larger scale but with better efficiency. These results give good confidence that the aero-acoustic characteristics on a very small scale, as presented in this research, can be used to accurately model full scale applications, and the further development of cavity control techniques.

Analytical Properties of Noise Generating Mechanisms in a Supersonic Jet Exhaust Flow

Analytical Properties of Noise Generating Mechanisms in a Supersonic Jet Exhaust Flow PDF Author: S. Paul Pao
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 76

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Computation of Supersonic Flow over Flying Configurations

Computation of Supersonic Flow over Flying Configurations PDF Author: Adriana Nastase
Publisher: Elsevier
ISBN: 008055699X
Category : Technology & Engineering
Languages : en
Pages : 425

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Book Description
Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. - Computational work and experimental results show the real-world application of computational results - Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations - Includes a fully optimized and integrated design for a proposed supersonic transport aircraft

The Generation and Radiation of Supersonic Jet Noise: Summary of supersonic jet noise studies

The Generation and Radiation of Supersonic Jet Noise: Summary of supersonic jet noise studies PDF Author:
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 50

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Aeroacoustics of Flight Vehicles

Aeroacoustics of Flight Vehicles PDF Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620

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Book Description