Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 398
Book Description
High Temperature Effects in Aircraft Structures
Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 398
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 398
Book Description
High Temperature Effects in Aircraft Structures
Author: Nicholas John Hoff
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 357
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 357
Book Description
High Temperature Effects in Aircraft Structure. Editor, Nicholas John Hoff, Etc
Author: Advisory Group for Aerospace Research and Development (NORTH ATLANTIC TREATY ORGANIZATION)
Publisher:
ISBN:
Category :
Languages : en
Pages : 357
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 357
Book Description
High Temperatures in Aeronautics
Author: Carlo Ferrari
Publisher: Elsevier
ISBN: 1483155021
Category : Technology & Engineering
Languages : en
Pages : 472
Book Description
High Temperatures in Aeronautics is a compilation of the proceedings of the Symposium on High Temperatures in Aeronautics held in Turin, Italy, on September 10-12, 1962. The symposium provided a forum to discuss the applications of high temperatures in aeronautics and covers topics ranging from supersonic combustion to non-equilibrium flow through a nozzle, along with similarity parameters in radiation gas-dynamics and photoionization upstream of a strong shock wave. This volume is comprised of 17 chapters and begins with an overview of the effects and consequences of high temperature in aeronautics, followed by an analysis of experimental results for the dissociation of diatomic gases. A theoretical and experimental investigation of mixing and supersonic combustion is then presented, focusing on inviscid flow fields with a finite rate chemistry for a hydrogen-air reaction. Turbulent mixing for flows with large density gradients having no chemical reaction is also considered, and the results of experiments in supersonic combustion are discussed. Subsequent chapters deal with silicon nitride, its properties, and its potential use at elevated temperatures; materials problems at high temperature; and the corrosion of refractory alloys by oil ash containing vanadium. This monograph will be of interest to students, engineers, and experimental workers in the fields of astronautics and aeronautical engineering.
Publisher: Elsevier
ISBN: 1483155021
Category : Technology & Engineering
Languages : en
Pages : 472
Book Description
High Temperatures in Aeronautics is a compilation of the proceedings of the Symposium on High Temperatures in Aeronautics held in Turin, Italy, on September 10-12, 1962. The symposium provided a forum to discuss the applications of high temperatures in aeronautics and covers topics ranging from supersonic combustion to non-equilibrium flow through a nozzle, along with similarity parameters in radiation gas-dynamics and photoionization upstream of a strong shock wave. This volume is comprised of 17 chapters and begins with an overview of the effects and consequences of high temperature in aeronautics, followed by an analysis of experimental results for the dissociation of diatomic gases. A theoretical and experimental investigation of mixing and supersonic combustion is then presented, focusing on inviscid flow fields with a finite rate chemistry for a hydrogen-air reaction. Turbulent mixing for flows with large density gradients having no chemical reaction is also considered, and the results of experiments in supersonic combustion are discussed. Subsequent chapters deal with silicon nitride, its properties, and its potential use at elevated temperatures; materials problems at high temperature; and the corrosion of refractory alloys by oil ash containing vanadium. This monograph will be of interest to students, engineers, and experimental workers in the fields of astronautics and aeronautical engineering.
Effects of Temperature and Time on Aircraft and Missile Structures
Author: Stanford University. Department of Aeronautical Engineering
Publisher:
ISBN:
Category :
Languages : en
Pages : 102
Book Description
A survey is made of the new problems introduced in the structural analysis of airplanes and missiles by the high temperatures caused by aerodynamic heating. Thermal stresses, thermal buckling, the effect of creep on stress distribution and stability, and ablation are discussed and special attention is paid to the behavior of the pure shells used in missiles. It is concluded that the modern structural analyst must acquire a knowledge of many disciplines that were of no interest to his predecessor working before World War II. Among these disciplines are thermodynamics, metallurgy, and the physics of the solid state. In all the new problems two parameters appear that did not enter classical structural analysis. The first is temperature which is the cause of all the difficulties of the modern structural designer and analyst. The second is time, because at high temperatures no structure can carry loads for indefinitely long periods. One of the most important tasks of the analyst of missiles is the determination of the lifetime of the structure. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 102
Book Description
A survey is made of the new problems introduced in the structural analysis of airplanes and missiles by the high temperatures caused by aerodynamic heating. Thermal stresses, thermal buckling, the effect of creep on stress distribution and stability, and ablation are discussed and special attention is paid to the behavior of the pure shells used in missiles. It is concluded that the modern structural analyst must acquire a knowledge of many disciplines that were of no interest to his predecessor working before World War II. Among these disciplines are thermodynamics, metallurgy, and the physics of the solid state. In all the new problems two parameters appear that did not enter classical structural analysis. The first is temperature which is the cause of all the difficulties of the modern structural designer and analyst. The second is time, because at high temperatures no structure can carry loads for indefinitely long periods. One of the most important tasks of the analyst of missiles is the determination of the lifetime of the structure. (Author).
Effects of Temperature-time-stress Histories on the Mechanical Properties of Aircraft Structural Metallic Materials
Author: C. D. Brownfield
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 118
Book Description
Publisher:
ISBN:
Category : Alloys
Languages : en
Pages : 118
Book Description
Thermal Structures for Aerospace Applications
Author: Earl Arthur Thornton
Publisher: AIAA
ISBN: 9781600861260
Category : Aerothermodynamics
Languages : en
Pages : 508
Book Description
Publisher: AIAA
ISBN: 9781600861260
Category : Aerothermodynamics
Languages : en
Pages : 508
Book Description
Composite Materials for Aircraft Structures
Author: Alan A. Baker
Publisher: AIAA
ISBN: 9781600860409
Category : Airplanes
Languages : en
Pages : 626
Book Description
Publisher: AIAA
ISBN: 9781600860409
Category : Airplanes
Languages : en
Pages : 626
Book Description
Investigation of Thermal Effects on Structural Fatigue
Author: Douglas Aircraft Company
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 224
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 224
Book Description
The Effects of Elevated Temperatures on Aircraft Structures
Author: Frederick V. Pohle
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description