Author: Helmut F. Bauer
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 132
Book Description
Theory of the Fluid Oscillations in a Circular Cylindrical Ring Tank Partially Filled with Liquid
Author: Helmut F. Bauer
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 132
Book Description
NASA Technical Note
The Coupled Dynamic Response of a Tank Partially Filled with a Liquid and Undergoing Free and Forced Planar Oscillations
Author: David G. Stephens
Publisher:
ISBN:
Category : Dynamics
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Dynamics
Languages : en
Pages : 56
Book Description
Propulsion Re-Entry Physics
Author: MichaĆ Lunc
Publisher: Elsevier
ISBN: 1483184323
Category : Technology & Engineering
Languages : en
Pages : 613
Book Description
Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.
Publisher: Elsevier
ISBN: 1483184323
Category : Technology & Engineering
Languages : en
Pages : 613
Book Description
Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.
Structural Dynamics of High Speed Flight
Fluid Oscillations in the Containers of a Space Vehicle and Their Influence Upon Stability
Author: Helmut F. Bauer
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 168
Book Description
With the increasing size of space vehicles and their larger diameters which lower the natural frequencies of the propellants, the effects of propellant sloshing especially since at launch a very large amount of the total weight is in the form of liquid propellant. With increasing diameters the eigenfrequencies of the propellant become smaller and shift closer to the control frequency of the space vehicle. Furthermore, the oscillating propellant masses and the corresponding forces increase considerably. A relatively simple means of avoiding strong dynamic coupling can be achieved by subdivision of the container by radial or circular walls. This results in smaller sloshing masses and higher eigenfrequencies. Another possibility is the clustering of tanks with small diameters which has the disadvantage of a weight penalty. For stability investigations the influence of the oscillating propellant has to be known. For this reason forces and moments of the propellant with a free fluid surface in a container of circular ring sector cross section performing forced oscillations must be determined. This will be performed with the assumption of irrotational, frictionless, and incompressible liquid. Linear equivalent damping is introduced with the help of a mechanical model describing the fluid motion. It has to be determined by experiments.
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 168
Book Description
With the increasing size of space vehicles and their larger diameters which lower the natural frequencies of the propellants, the effects of propellant sloshing especially since at launch a very large amount of the total weight is in the form of liquid propellant. With increasing diameters the eigenfrequencies of the propellant become smaller and shift closer to the control frequency of the space vehicle. Furthermore, the oscillating propellant masses and the corresponding forces increase considerably. A relatively simple means of avoiding strong dynamic coupling can be achieved by subdivision of the container by radial or circular walls. This results in smaller sloshing masses and higher eigenfrequencies. Another possibility is the clustering of tanks with small diameters which has the disadvantage of a weight penalty. For stability investigations the influence of the oscillating propellant has to be known. For this reason forces and moments of the propellant with a free fluid surface in a container of circular ring sector cross section performing forced oscillations must be determined. This will be performed with the assumption of irrotational, frictionless, and incompressible liquid. Linear equivalent damping is introduced with the help of a mechanical model describing the fluid motion. It has to be determined by experiments.
NASA Technical Report
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 832
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 832
Book Description
Shock and Vibration Environment
Author: Wendell L. Hercules
Publisher:
ISBN:
Category : Environmental engineering
Languages : en
Pages : 162
Book Description
Publisher:
ISBN:
Category : Environmental engineering
Languages : en
Pages : 162
Book Description
Applied Mechanics Reviews
An Investigation of the Natural Frequencies and Mode Shapes of Liquids in Oblate Spheroidal Tanks
Author: H. Wayne Leonard
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 28
Book Description