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Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics / Rudolf HERMANN
Titre : Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics Type de document : texte imprimé Auteurs : Rudolf HERMANN Editeur : Minneapolis-Honeywell Regulator Company, Ltd. Année de publication : 1956 Importance : 378 p. Note générale : Preface
Table of Contents
Appendix of Numerical Tables
References
Terminology
Index
List of TablesCatégories : Aérodynamique Index. décimale : 533.6 Aérodynamique Résumé : Various Diffuser Types, Their Functions and Applications in Supersonic Aerodynamics
Diffuser with the Normal Shock in Front : Flow Process, Efficiency and the Starting or Swallowing Process in One-dimensional Analysis
Diffuser with the Normal Shock Swallowed : Flow Process and Efficiency in One-dimensionam Analysis
The Two-dimensional Symmetric Multiple Shock Diffuser with a Wedge of Constant Angle Installes in a Duct
The Two-dimensional Multiple Shock Inlet Diffuser with Equal Upper and Lower Wedge Angles
Analysis of Two-dimensional Multiple Shock System for Optimum Pressure Recovery
Comparative Evaluation of Two-dimentsional Unsymmetric Multiple Shock Inlet Diffusers Composed of Wedges with Unequal Angles or Angular Steps
The Axially Symmetric Spike Inlet Diffuser - Basic Analysis of On-design Mach Number Operation
The Axially Symmetric Spike Inlet Diffuser - Experimental Data and Comparison with AnalysisExemplaires (1)
Code-barres Cote Support Localisation Section Disponibilité B00007284 533.6 HER Ouvrage BIBLIOTHÈQUE - ACCÈS LIBRE 500 - Sciences - Mathématiques Disponible