Calibration of a Shock Tube by Analysis of the Particle Trajectories [microform]

Calibration of a Shock Tube by Analysis of the Particle Trajectories [microform] PDF Author: Brian Thomas Whitten
Publisher: National Library of Canada = Bibliothèque nationale du Canada
ISBN:
Category : Gas dynamics
Languages : en
Pages : 394

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Book Description
It can be shown that for the complete description of all the physical parameters in the flow behind an imtermediate strength unsteady shock, a knowledge of the particle trajectories within the flow is sufficient. This principle has been applied to determine the variation of the physical parameters throughout the length of a conventional shock tube. The particle trajectories were obtained by the high speed photography of cigarette smoke tracers, placed at 10 cm. intervals along the tube. By applying the conservation of mass equation to the particle trajectory data, the density variation was obtained throughout the flow including the rarefaction wave from the end of the compression chamber and behind the first reflected shock from the closed end of the expansion chamber. By means of the Rankine-Hugoniot relation, the pressures immediately behind the incident and reflected shock fronts were calculated, and by assuming isentropic flow between shocks along any particle trajectory, the complete pressure variation was determined. The temperature and local sound speed were subsequently calculated at all points and the particle velocities were determined from the time derivative of the particle trajectories. A complete mapping of all the parameters in the shock tube was thus obtained using a single photographic technique, which is simpler than previous methods.

Calibration of a Shock Tube by Analysis of the Particle Trajectories [microform]

Calibration of a Shock Tube by Analysis of the Particle Trajectories [microform] PDF Author: Brian Thomas Whitten
Publisher: National Library of Canada = Bibliothèque nationale du Canada
ISBN:
Category : Gas dynamics
Languages : en
Pages : 394

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Book Description
It can be shown that for the complete description of all the physical parameters in the flow behind an imtermediate strength unsteady shock, a knowledge of the particle trajectories within the flow is sufficient. This principle has been applied to determine the variation of the physical parameters throughout the length of a conventional shock tube. The particle trajectories were obtained by the high speed photography of cigarette smoke tracers, placed at 10 cm. intervals along the tube. By applying the conservation of mass equation to the particle trajectory data, the density variation was obtained throughout the flow including the rarefaction wave from the end of the compression chamber and behind the first reflected shock from the closed end of the expansion chamber. By means of the Rankine-Hugoniot relation, the pressures immediately behind the incident and reflected shock fronts were calculated, and by assuming isentropic flow between shocks along any particle trajectory, the complete pressure variation was determined. The temperature and local sound speed were subsequently calculated at all points and the particle velocities were determined from the time derivative of the particle trajectories. A complete mapping of all the parameters in the shock tube was thus obtained using a single photographic technique, which is simpler than previous methods.

Calibration of a Shock Tube by Analysis of the Particle Trajectories

Calibration of a Shock Tube by Analysis of the Particle Trajectories PDF Author: Brian Thomas Whitten
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 0

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Book Description
It can be shown that for the complete description of all the physical parameters in the flow behind an imtermediate strength unsteady shock, a knowledge of the particle trajectories within the flow is sufficient. This principle has been applied to determine the variation of the physical parameters throughout the length of a conventional shock tube. The particle trajectories were obtained by the high speed photography of cigarette smoke tracers, placed at 10 cm. intervals along the tube. By applying the conservation of mass equation to the particle trajectory data, the density variation was obtained throughout the flow including the rarefaction wave from the end of the compression chamber and behind the first reflected shock from the closed end of the expansion chamber. By means of the Rankine-Hugoniot relation, the pressures immediately behind the incident and reflected shock fronts were calculated, and by assuming isentropic flow between shocks along any particle trajectory, the complete pressure variation was determined. The temperature and local sound speed were subsequently calculated at all points and the particle velocities were determined from the time derivative of the particle trajectories. A complete mapping of all the parameters in the shock tube was thus obtained using a single photographic technique, which is simpler than previous methods.

Particle Trajectory Analysis of a Two-dimensional Shock Tube Flow [microform]

Particle Trajectory Analysis of a Two-dimensional Shock Tube Flow [microform] PDF Author: David Keith Walker
Publisher: National Library of Canada = Bibliothèque nationale du Canada
ISBN:
Category : Gas dynamics
Languages : en
Pages : 176

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Book Description
The physical properties within the two-dimensional flow produced by the reflection of a plane shock of intermediate strength at a wedge, have been determined by analysis of the particle trajectories. The particle trajectories were obtained by high speed photography of smoke tracers within the flow. Trajectories were determined for different initial positions of the tracers relative to the wedge. The conservation of mass equation was used to determine the density at points within the flow. A knowledge of the shock configurations within the flow, together with the Rankins-Hugoniot equation, was used to determine the pressure immediately behind the incident and reflected shocks. The isentropic equation of state was used to determine the pressure after the passage of the reflected shock. The pressure determined in this manner agreed, within the limits of experimental error, with that obtained using a piezo-electric transducer. The temperature, velocity of sound, and particle velocity at points within the flow were also determined.

Particle Trajectory Analysis of a Two-dimensional Shock Tube Flow

Particle Trajectory Analysis of a Two-dimensional Shock Tube Flow PDF Author: David Keith Walker
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 0

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Book Description
The physical properties within the two-dimensional flow produced by the reflection of a plane shock of intermediate strength at a wedge, have been determined by analysis of the particle trajectories. The particle trajectories were obtained by high speed photography of smoke tracers within the flow. Trajectories were determined for different initial positions of the tracers relative to the wedge. The conservation of mass equation was used to determine the density at points within the flow. A knowledge of the shock configurations within the flow, together with the Rankins-Hugoniot equation, was used to determine the pressure immediately behind the incident and reflected shocks. The isentropic equation of state was used to determine the pressure after the passage of the reflected shock. The pressure determined in this manner agreed, within the limits of experimental error, with that obtained using a piezo-electric transducer. The temperature, velocity of sound, and particle velocity at points within the flow were also determined.

Calibration of Shock Tubes for Studying Aerodynamic Loading

Calibration of Shock Tubes for Studying Aerodynamic Loading PDF Author: John M. Dewey
Publisher:
ISBN:
Category :
Languages : en
Pages : 4

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Book Description
In a simple shock tube the physical parameters behind the shock cannot be determined from the measurement of a single parameter, such as the pressure, because of uncertainties about the state of the gas in this region. Results are shown which illustrate two causes of this uncertainty: (A) the mixing of the driver and expansion chamber gases, and (B) the variation of the shock strength along the tube. The problem can be overcome by observing the particle trajectories throughout the tube. This is done by high-speed photography of smoke tracers, and it is shown that the technique permits a determination of all the physical parameters of the flow without reference to other measurements. (Author).

Measurement of Frequency Response of Pressure Gauges by a High-pressure Shock Tube Technique

Measurement of Frequency Response of Pressure Gauges by a High-pressure Shock Tube Technique PDF Author: S. P. Pfaff
Publisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 30

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Book Description


The Calibration and Interpretation of Recorded Shock-tube Pressure Data Using Piezoelectric Sensors

The Calibration and Interpretation of Recorded Shock-tube Pressure Data Using Piezoelectric Sensors PDF Author: C. W. Hicks
Publisher:
ISBN:
Category :
Languages : en
Pages : 78

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Book Description
This report is intended to serve as a guide, or basis, for the calibration and analysis of recorded pressure data. Many of the techniques and areas covered are also applicable to other types of gages; i.e., strain, velocity, acceleration, etc. Photographs of typical shock-tube data are generously used to familiarize the reader with the actual appearance of the true pressure pulse which has been modulated by the effects of resonance, overshoot, groundloops, inadequate bandwidth, and poor gage isolation.

Shock-tube Flow Analysis with a Dimensionless Velocity Number

Shock-tube Flow Analysis with a Dimensionless Velocity Number PDF Author: N. Muniswamy Reddy
Publisher:
ISBN:
Category : Measurement
Languages : en
Pages : 28

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Book Description
Shock tube flow analysis with dimensionless velocity number.

Velocity Calibration of a Shock Tube

Velocity Calibration of a Shock Tube PDF Author: Robert Bernard Ludford Taylor
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 40

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Book Description


Canadiana

Canadiana PDF Author:
Publisher:
ISBN:
Category : Canada
Languages : en
Pages : 1232

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Book Description