| Vorliegende Sprache |
eng |
| Hinweise auf parallele Ausgaben |
391208128 Buchausg.: ‡Bose, Tarit, 1939 - : Airbreathing propulsion |
| ISBN |
978-1-4614-3531-0 |
| Name |
Bose, Tarit |
| T I T E L |
Airbreathing Propulsion |
| Zusatz zum Titel |
An Introduction |
| Verlagsort |
New York, NY |
| Verlag |
Springer New York |
| Erscheinungsjahr |
2012 |
| 2012 |
| Umfang |
Online-Ressource (IX, 309 p. 98 illus., 9 illus. in color, digital) |
| Reihe |
Springer Aerospace Technology |
| Notiz / Fußnoten |
Description based upon print version of record |
| Weiterer Inhalt |
Airbreathing Propulsion; Preface; Contents; Chapter 1: Introduction; 1.1 Historical; 1.2 Comparison Among Piston Engines, Turboprops, and Turbojets; 1.3 Thermal Efficiency, Overall Efficiency, and Specific Fuel Consumption; 1.4 Fuel Combustion with Air; 1.4.1 Future Fuels; 1.5 Specific Impulse and Range; 1.6 Some Selected Aircraft Engines and Future Trends; 1.7 Exercises; Chapter 2: Thermodynamic Ideal Cycle Analysis; 2.1 Propeller-Driven Engines; 2.1.1 Ideal Otto Cycle; 2.1.2 Ideal Diesel Cycle; 2.1.3 Force and Moment Analysis for Piston Engines. 2.1.4 An Interactive Code for Performance of Otto/Diesel Engines2.1.5 Ideal Turboprop Cycles; 2.2 Jet Engines; 2.2.1 Ideal Ramjet Cycle; 2.2.2 Ideal Straight-Jet Cycle with Afterburner; 2.2.3 Ideal Bypass Jet Cycle with Afterburner; 2.2.4 Ideal Fanjet Cycle with Afterburner; 2.2.5 An Interactive Computer Program for Ideal Jet Engine Analysis (PAGIC); 2.3 Exercises; Chapter 3: Friction, Work, and Heat Addition in a One-Dimensional Channel; 3.1 Discussion on Efficiencies; 3.1.1 Diffuser Efficiency; 3.1.2 Combustion Chamber Efficiencies; 3.1.3 Exhaust Nozzle Efficiencies. 3.2 Compressor and Turbine Stage and Polytropic Efficiencies3.3 Heating Factor During Compression and Expansion; 3.4 Exercises; Chapter 4: Flow Through a Turbomachine; 4.1 Elementary Theory of a Stage; 4.2 Reaction and Shape of Blades; 4.3 Exercises; Chapter 5: Estimating Losses; 5.1 Estimating Losses for Axial Turbomachinery Blades; 5.1.1 Losses in an Axial Turbine; 5.1.2 Losses in an Axial Compressor; 5.2 Estimating Losses for Centrifugal Compressors; 5.3 Other Losses; 5.4 Slip Factor, Diffusion Factor, and Blockage Factor; 5.5 Exercises; Chapter 6: Similarity Rules (on Design Condition). 6.1 ExerciseChapter 7: Axial Compressors and Turbines; 7.1 Equation of Radial Equilibrium; 7.2 Selection of Airfoil Profile for Axial Machines; 7.3 Calculating Potential Flow in a Blade Cascade; 7.3.1 Simple Vortex Theory; 7.3.2 Exact Calculation of Potential Flow; 7.3.3 Numerical Calculation of Flow; 7.3.4 Design of Circular Arc Blades; 7.4 Multiple Axial Compressors; 7.5 Two Examples; 7.5.1 Example 1; 7.5.2 Example 2; Chapter 8: Centrifugal Compressor; 8.1 Calculation of a Centrifugal Compressor; Chapter 9: Off-Design Running of Aircraft Gas Turbines. 9.1 Analytical Calculation of Performance Map of a Multistage Axial Compressor9.2 Equilibrium Running Condition; 9.3 Surge and Stall; 9.3.1 Casing Treatment for Rotors; 9.4 Matching of Running of Turbine and Compressor; 9.5 Fuel and Engine Controls; 9.6 Exercises; Chapter 10: Propeller Aerodynamics; 10.1 Axial Momentum Theory; 10.2 Blade Element Theory; 10.3 Exercise; Chapter 11: Materials and Structural Problems; 11.1 Materials Problems; 11.2 Normal Stress Analysis; 11.3 Bending Stress (for Axial Blades); 11.4 Torsional Stress; 11.5 Oscillation of Blades; 11.5.1 Bending Oscillation. 11.5.2 Torsion Self-Oscillation Frequency |
| Titelhinweis |
Buchausg.: ‡Bose, Tarit, 1939 - : Airbreathing propulsion |
| ISBN |
ISBN 978-1-4614-3532-7 |
| Klassifikation |
TRP |
| TTDS |
| TEC002000 |
| 629.13435 |
| 629.1 |
| 629.13335 |
| TL787-4050.22 |
| ZO 7270 |
| Kurzbeschreibung |
Airbreathing Propulsion covers the physics of combustion, fluid and thermo-dynamics, and structural mechanics of airbreathing engines, including piston, turboprop, turbojet, turbofan, and ramjet engines. End-of-chapter exercises allow the reader to practice the fundamental concepts behind airbreathing propulsion, and the included PAGIC computer code will help the reader to examine the relationships between the performance parameters of different engines. Large amounts of data have on many different piston, turbojet, and turboprop engines have been compiled for this book and are included as an appendix. This textbook is ideal for senior undergraduate and graduate students studying aeronautical engineering, aerospace engineering, and mechanical engineering. |
| 1. Schlagwortkette |
Luftstrahltriebwerk |
| ANZEIGE DER KETTE |
Luftstrahltriebwerk |
| SWB-Titel-Idn |
367686570 |
| Signatur |
Springer E-Book |
| Bemerkungen |
Elektronischer Volltext - Campuslizenz |
| Elektronische Adresse |
$uhttp://dx.doi.org/10.1007/978-1-4614-3532-7 |
| Internetseite / Link |
Volltext |
| Siehe auch |
Volltext |
| Siehe auch |
Cover |
