
High Temperatures in Aeronautics
Proceedings of the Symposium Held in Turin to Celebrate the 50th Anniversary of the Laboratorio di Aeronautica, Politecnico di Torino, 10-12 September 1962
- 472 pages
- English
- PDF
- Available on iOS & Android
High Temperatures in Aeronautics
Proceedings of the Symposium Held in Turin to Celebrate the 50th Anniversary of the Laboratorio di Aeronautica, Politecnico di Torino, 10-12 September 1962
About this book
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.
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Table of contents
- Front Cover
- High Temperatures in Aeronautics
- Copyright Page
- Table of Contents
- PREFAZIONE
- List of Participants
- Adesioni
- Proceedings
- CHAPTER 1. EFFETTI DELLE ALTE TEMPERATURE IN AERODINAMICA
- CHAPTER 2. ANALISI DI ALCUNI RISULTATI SPERIMENTALI SULLA DISSOCIAZIONE DI GAS BIATOMICI NEL TUBO D'URTO
- CHAPTER 3. RICERCHE DI AEROTERMODINAMICA PRESSO L'ISTITUTO DI MACCHINE E MOTORI PER AEROMOBILIDEL POLITECNICO DI TORINO
- CHAPTER 4. THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SUPERSONIC COMBUSTION
- CHAPTER 5. MOTI LINEARIZZATI NON IN EQUILIBRIO DI MISCELE BI-REAGENTI
- CHAPTER 6. NON-EQUILIBRIUM FLOW THROUGH A NOZZLE
- CHAPTER 7. SIMILARITY PARAMETERS IN RADIATION GAS-DYNAMICS
- CHAPTER 7. RADIATIVE TRANSFER STUDIES AND OPACITY CALCULATIONS FOR HEATED GASES
- CHAPTER 8. PHOTOIONIZATION UPSTREAM OF A STRONG SHOCK WAVE
- CHAPTER 9. ETUDE DE CERTAINS JETS DE PLASMA
- CHAPTER 10. SUL MOTO DI UN FLUIDO ELETTRICAMENTE CONDUTTORE PER DATE CONDIZIONI DI DISTRIBUZIONE DELLA CORRENTE DI CONDUZIONE E DEI VORTICI
- CHAPTER 11. ESPERIMENTI DI PROPULSIONE ELETTRICA MEDIANTE MOTORI ELETTROTERMICI
- CHAPTER 12. FLAMBEMENT THERMIQUE DES COQUES CYLINDRIQUES CIRCULAIRES À PAROIS MINCES
- CHAPTER 13. PROBLEMI TERMICI DEL RIENTRO
- CHAPTER 14. SILICON NITRIDE: A REVIEW OF ITS PROPERTIES AND ATTRACTIVENESS FOR USE AT ELEVATED TEMPERATURES
- CHAPTER 15. MATERIALS PROBLEMS AT HIGH TEMPERATURE
- CHAPTER 16. LA CORROSIONE DI LEGHE REFRATTARIE DA PARTE DI CENERI DI PETROLIO CONTENENTI VANADIO
- CHAPTER 17. CONSIDERAZIONI SULLE CARATTERISTICHE E SULLE PROVE MECCANICHE DI MATERIALIPER LE COSTRUZIONI MISSILISTICHE