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Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley
| Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| Autore | Dranovsky Mark L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (342 p.) |
| Disciplina | 621.43/56 |
| Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-690-5
1-60086-471-6 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
| Record Nr. | UNINA-9910457203903321 |
Dranovsky Mark L
|
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley
| Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| Autore | Dranovsky Mark L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (342 p.) |
| Disciplina | 621.43/56 |
| Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
| ISBN |
1-60086-690-5
1-60086-471-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
| Record Nr. | UNINA-9910781700303321 |
|
Dranovsky Mark L
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley
| Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
| Autore | Dranovsky Mark L |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
| Descrizione fisica | 1 online resource (342 p.) |
| Disciplina | 621.43/56 |
| Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
| ISBN |
1-60086-690-5
1-60086-471-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
| Record Nr. | UNINA-9910817251603321 |
|
Dranovsky Mark L
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Digital computer program for analysis of chugging instabilities / / by John R. Szuch
| Digital computer program for analysis of chugging instabilities / / by John R. Szuch |
| Autore | Szuch John R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1970 |
| Descrizione fisica | 1 online resource (76 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Rocket engines
Feed systems Liquid propellant rockets Rocket engines - Combustion Rockets (Aeronautics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716552603321 |
|
Szuch John R.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1970 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910136758203321 |
|
Wang Zhen-Guo
|
||
| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang
| Internal combustion processes of liquid rocket engines : modeling and numerical simulations / / Zhen-Guo Wang |
| Autore | Wang Zhen-Guo |
| Pubbl/distr/stampa | Singapore : , : Wiley, , 2016 |
| Descrizione fisica | 1 online resource (395 p.) |
| Disciplina | 629.47522 |
| Soggetto topico |
Liquid propellant rockets
Liquid propellant rocket engines |
| ISBN |
1-118-89005-1
1-118-89004-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page ; Copyright Page ; Contents; Preface; Chapter 1 Introduction ; 1.1 Basic Configuration of Liquid Rocket Engines; 1.1.1 Propellant Feed System; 1.1.2 Thrust Chamber; 1.2 Internal Combustion Processes of Liquid Rocket Engines; 1.2.1 Start and Shutdown; 1.2.2 Combustion Process; 1.2.3 Performance Parameters in Working Process; 1.3 Characteristics and Development History of Numerical Simulation of the Combustion Process in Liquid Rocket Engines; 1.3.1 Benefits of Numerical Simulation of the Combustion Process in Liquid Rocket Engines
1.3.2 Main Contents of Numerical Simulations of Liquid Rocket Engine Operating Process1.3.3 Development of Numerical Simulations of Combustion Process in Liquid Rocket Engines; 1.4 Governing Equations of Chemical Fluid Dynamics; 1.5 Outline of this Book; References; Chapter 2 Physical Mechanism and Numerical Modeling of Liquid Propellant Atomization ; 2.1 Types and Functions of Injectors in a Liquid Rocket Engine; 2.2 Atomization Mechanism of Liquid Propellant; 2.2.1 Formation of Static Liquid Droplet; 2.2.2 Breakup of Cylindrical Liquid Jet; 2.2.3 Liquid Sheet Breakup 2.2.4 Droplet Secondary Breakup2.3 Characteristics of Atomization in Liquid Rocket Engines; 2.3.1 Distribution Function of the Droplet Size; 2.3.2 Mean Diameter and Characteristic Diameter; 2.3.3 Measurement of Spray Size Distribution; 2.4 Atomization Modeling for Liquid Rocket Engine Atomizers; 2.4.1 Straight-flow Injector; 2.4.2 Centrifugal Injector; 2.4.3 Impinging-stream Injectors; 2.4.4 Coaxial Shear Injector; 2.4.5 Coaxial Centrifugal Injectors; 2.5 Numerical Simulation of Liquid Propellant Atomization; 2.5.1 Theoretical Models of Liquid Propellant Atomization; 2.5.2 Quasi-fluid Models 2.5.3 Particle Trajectory Models2.5.4 Simulation of Liquid Jet Atomization Using Interface Tracking Method; 2.5.5 Liquid Jet Structure - Varying Flow Conditions; References; Chapter 3 Modeling of Droplet Evaporation and Combustion ; 3.1 Theory for Quasi-Steady Evaporation and Combustion of a Single Droplet at Atmospheric Pressure; 3.1.1 Quasi-Steady Evaporation Theory for Single Droplet in the Static Gas without Combustion; 3.1.2 Quasi-Steady Evaporation Theory for Droplet in a Static Gas with Combustion; 3.1.3 Non-Combustion Evaporation Theory for a Droplet in a Convective Flow 3.1.4 Evaporation Theory for a Droplet in a Convective Medium with Combustion3.2 Evaporation Model for a Single Droplet under High Pressure; 3.2.1 ZKS Droplet High Pressure Evaporation Theory; 3.2.2 Application of the Liquid Activity Coefficient to Calculate the Gas-Liquid Equilibrium at a High Pressure; 3.3 Subcritical Evaporation Response Characteristics of Propellant Droplet in Oscillatory Environments; 3.3.1 Physical Model; 3.3.2 Examples and the Analysis of Results; 3.4 Multicomponent Fuel Droplet Evaporation Model; 3.4.1 Simple Multicomponent Droplet Evaporation Model 3.4.2 Continuous Thermodynamics Model of Complex Multicomponent Mixture Droplet Evaporation |
| Record Nr. | UNINA-9910830290403321 |
|
Wang Zhen-Guo
|
||
| Singapore : , : Wiley, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910457165203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910781420203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang
| Liquid rocket engine combustion instability [[electronic resource] /] / edited by William E. Anderson and Vigor Yang |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (580 p.) |
| Disciplina | 629.47522 |
| Altri autori (Persone) | YoungVigor |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion |
| ISBN |
1-60086-637-9
1-60086-418-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. |
| Record Nr. | UNINA-9910811648603321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid rockets and propellants [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society ... / / edited by Loren E. Bollinger, Martin Goldsmith, Alexis W. Lemmon, Jr
| Liquid rockets and propellants [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society ... / / edited by Loren E. Bollinger, Martin Goldsmith, Alexis W. Lemmon, Jr |
| Pubbl/distr/stampa | New York, : Academic Press, 1960 |
| Descrizione fisica | 1 online resource (698 p.) |
| Disciplina | 629.4222 |
| Altri autori (Persone) |
BollingerLoren E
GoldsmithMartin LemmonAlexis W |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Liquid propellant rockets |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-475-9
1-60086-256-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Liquid Rockets Committee and Propellants and Combustion Committee""; ""Contributors to Volume 2""; ""Preface""; ""Contents""; ""A. Simulated High-Altitude Testing of Rockets""; ""Experimental Investigation of Exhaust Diffusers for Rocket Engines""; ""Summary of Experience in the Use of Exhaust Diffusers for Rocket Testing""; ""Short Diffuser for Testing Rocket Nozzles""; ""A Large Rocket Ejector System""; ""Development of an Exhaust Diffuser for Ground Testing Rocket Engines""; ""B. Instrumentation for Combustion Instability""
""Instrumentation for Research on Combustion Instability in Solid-Propellant Rocket Motors""""Some Instrumentation for Combustion Stability Research""; ""An Integrated Combustion Instability Recording and Analysis Installation""; ""High Frequency Pressure Instrumentation for Rocket Instability Studies""; ""Instrumentation for Studies of Unstable Burning Phenomena""; ""C. Liquid Propellant Combustion""; ""Monodisperse Spray Deflagration""; ""A Two-Wavelength Interferometric Technique for the Study of Vaporization and Combustion of Fuels"" ""An Experimental Study of RP-1, UDMH and N[sub(2)]H[sub(4)] Single-Droplet Burning in Air and in Oxygen""""D. Reaction Kinetics""; ""The Reaction of Diborane and Oxygen under Explosive and Pre-Explosive Conditions""; ""Consideration of Hydrazine Decomposition""; ""Detonability of Ozone and Nitric Oxide""; ""Nonequilibrium Chemical Recombination Effects in Exhaust Nozzle Flow: An Approximate Method""; ""Spectroscopic Techniques for the Determination of Flame Temperatures: Total Radiation Techniques""; ""Production and Properties of Liquid Ozone and Liquid Ozone-Oxygen Mixtures, A Review"" ""E. Propellant Selection""""Liquid Propellant Comparison Based on Vehicle Performance""; ""Comparative Applicability of Storable Propellants: Effects of Specific Impulse and Density""; ""F. Rocket Engine Design""; ""Investigation of a Gas-Driven Jet Pump for Rocket Engines""; ""Analysis of Pressure Feasibility Limits in Regenerative Cooling of Combustion Chambers for Large-Thrust Rockets""; ""Fabrication, Structural and Heat Transfer Considerations of Electroformed Rocket Nozzles""; ""Design of Catalyst Packs for the Decomposition of Hydrogen Peroxide""; ""Variable Thrust Rocket Engines"" ""Starting Transients of Hypergolic Bipropellant Rockets""""Analysis of a New Concept Rocket Nozzle"" |
| Record Nr. | UNINA-9910457223003321 |
| New York, : Academic Press, 1960 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
