Author: Planjery V. SankaranarayanaPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 150
Book Description
Unsteady Supersonic Flow from a Tube with Continuous Energy Release
Author: Planjery V. SankaranarayanaPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 150
Book Description
Unsteady Supersonic Flow from a Tube
Author: C. J. ChenPublisher:
ISBN:
Category :
Languages : en
Pages : 89
Book Description
The strength of the shock wave in the vicinity of a gun is predicted. The energy release is considered to be a function of time. As the shock wave reaches the point of analysis the energy is still being released. It is found that the energy release by the after-flashing will not significantly alter the shock strength but will affect the flow behind the shock wave. The pressure behind the shock wave will decrease slower if the energy is released continuously. The strength of the shock wave in general decreases with increase of the length of tube and is proportional to the total energy released.
Study of Unsteady Flow Disturbances of Large and Small Amplitudes Moving Through Supersonic Or Subsonic Steady Flows
Author: Robert V. HessPublisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 108
Book Description
In Part 1 a point-by-point method is developed for the calculation of unsteady flows through tubes with variable cross sections containing strong shocks and large temperature contact discontinuities. In Part 2 calculations are made of the flow pattern created by bursting into a vacuum of a diaphragm at the minimum section of a supersonic nozzle without a second throat. In Part 3 integral relationships are developed which describe as a whole the behavior of unsteady flow disturbances of large and small amplitudes. The invariant integrals are the conservation laws for the potential, pulse area, mass, and energy.
A Study of Unsteady Shock-induced Supersonic Flow Over a Wedge Mounted in a Shock Tube
Author: Dennis Frederick KabelePublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 188
Book Description
The Potential Theory of Unsteady Supersonic Flow
Author: John Wilder MilesPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 244
Book Description
The Potential Theory of Unsteady Supersonic Flow
Author: John Wilder MilesPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 220
Book Description
The Potential Theory of Unsteady Supersonic Flow
Author: pseud ArmigerPublisher:
ISBN:
Category :
Languages : en
Pages : 220
Book Description
Unsteady Supersonic Flow Over a Cone with a Blunted Tip
Author: G. F. TELENINPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
Unsteady Supersonic Flow Past a Circular Cone Pitching and Plunging in a Plane
Author: Henry Wing H. KanPublisher:
ISBN:
Category :
Languages : en
Pages : 192
Book Description
INVESTIGATION OF THE UNSTEADY FLOW AROUND BODIES BY A Current Moving Behind a Shock Wave
Author: K. E. BogoslovskiiPublisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
The results of an experimental investigation of unsteady supersonic flow past cylinders are presented. The purpose of the experiment was to determine the basic criteria characterizing an unsteady flow behind a two-dimensional shock wave having constant time parameters and to ascertain the correlation between the variable location of a reflected shock wave and the surface pressure on the body. The experiments were carried out by subjecting cylinders with flat and spherical bluntness to axisymmetrical and transverse flows in a shock tube. The range of the Mach numbers of the incident shock-waves was from 1.5 to 6. The magnitudes of maximum shock detachment distance at the stagnation point obtained were compared with available data and were found to be in good agreement. (Author).
