Culick, F. E. C.

English

Caltech Authors - Main

Oscillatory and unsteady processes in liquid rocket engines

A Comprehensive Review of Liquid-Propellant Instabilities in F-l En gines,&quot;

A Comprehensive Review of Liquid-Propellant Instabilities in F-l Engines,&quot;

A Note on Rayleigh's Criterion,&quot;

A Numerical Study of Nonlinear Instability Phenomena in Solid Rocket Motors,&quot;

A Shock Wave Model of Unstable Rocket Combustors,&quot;

A Simplified Computer Program for the Prediction of the Linear Stability Behavior of Liquid Propellant Combustors,&quot;

A Theoretical Study of Nonlinear Combustion Instability in Liquid-Propellant Rocket Engines,&quot;

A Theoretical Study of Nonlinear Combustion Instability: Longitudinal Mode,

A Theory of Unstable Combustion in Liquid Propellant Rocket Systems,&quot;

Aerodynamic Effects on Primary and Secondary Spray Breakup,&quot;

An Application of Dynamical Systems Theory to Nonlinear Com bustion Instabilities,&quot;

An Application of Dynamical Systems Theory to Nonlinear Combustion Instabilities,&quot;

Analysis of a Self-Sustained Thermally Driven Nonlinear Vibration &quot;

Analysis of Frequency Response Characteristics of Propellant Vaporization,&quot;

Analysis of the F-l Acoustic Liner,&quot;

Analysis ofn-Heptane Vaporization in Unstable Combustor With Traveling Transverse Oscillations,&quot;

Application of the Galerkin Method in the Solution of Nonlinear Axial Combustion Instability Problems in Liquid Rockets,&quot;

Behavior of Supercritical Nozzles Under Three-Dimensional Oscil latory Conditions,&quot; AGARDograph No.

Behavior of Supercritical Nozzles Under Three-Dimensional Oscillatory Conditions,&quot;

Coaxial Injectors, Atomization,&quot;

Combustion Instabilities in Liquid-Fueled Propulsion Systems - An Overview,&quot;

Combustion of Liquid-Fuel Droplets in Supercritical Condi tions,&quot;

Combustion of Liquid-Fuel Droplets in Supercritical Conditions,&quot;

Droplet Vaporization in High-Pressure Environments, I: Near Critical Conditions,&quot;

Etude de l'Effet POGO sur les Lanceurs

High Frequency Oscillations in Liquid Rockets,&quot;

Introduction to Nonlinear Mechanics,

Liquid Propellant Rockets,&quot;

Longitudinal Instability of Liquid Rockets Due to Propulsion Feedback (POGO),&quot;

Nonlinear Analysis of Solid Rocket Combustion Instability,&quot; Ultra systems, Inc., report prepared for the Air Force Rocket Propulsion Laboratory,

Nonlinear Analysis of Solid Rocket Combustion Instability,&quot; Ultrasystems, Inc., report prepared for the Air Force Rocket Propulsion Laboratory,

Nonlinear Behavior of Acoustic Waves in Combustion Chambers,&quot; Parts I and II,

Nonlinear Instability in Liquid-Propellant Rocket Engines,&quot;

Nonlinear Longitudinal Instability in Rocket Motors with Concentrated Combustion,&quot;

Nonlinear Longitudinal Instability in Rocket Motors,&quot;

Nonlinear Periodic Oscillations in Rocket Motors with Distributed Combustion,&quot;

Numerical Analysis of Nonlinear Longitudinal Combustion Instability in Metalized Solid-Propellant Rocket Motors,&quot;

On Strong Transverse Waves Without Shocks in a Circular Cylinder,&quot;

On the Existence and Stability of Limit Cycles for Longitudinal Acoustic Modes in a Combustion Chamber,&quot;

On the Existence and Stability of Limit Cycles for Traverse Acoustic Oscillations in a Cylindrical Combustion Chamber, I. Standing Modes,&quot;

Prediction of the Stability of Unsteady Motions in Solid Propellant Rocket Motors,&quot;

Pulsating Combustion,&quot;

Resolution du Probleme des Instabilities sur Ie Moteur Viking,&quot;

Rotating Flows in Acoustically Unstable Rocket Motors,

Software for Continuation Problems in Ordinary Differential Equa tions with Applications, Applied Ma.thematics Publication 217-50,

Software for Continuation Problems in Ordinary Differential Equations with Applications, Applied Ma.thematics Publication 217-50,

Some Recent Results for Nonlinear Acoustics in Combustion Chambers,&quot;

Sound Attentuation in a Condensing Vapor,&quot;

Stability of Flow in a Rocket Motor,&quot;

Standard Stability Prediction Method for Solid Rocket Motors, Axial Mode Computer Program, User's Manual,&quot; Software and Engineering Associates, Inc., report prepared for Air Force Rocket Propulsion Laboratory,

Supercritical Droplet Combustion and Related Transport Phenomena,&quot;

Supercritical Gas Discharge With High Frequency Oscillations,&quot;

The Explanation of Certain Acoustical Phenomena,&quot;

The Transfer Functions of Rocket Nozzles,&quot;

Theory of Liquid Propellant Rocket Combustion Instability and Its Experimental Verification,&quot;

Thermally Driven Nonlinear Oscillations in a Pipe with Traveling Shock Waves,&quot;

Vaporization Response of Fuel Droplet in Oscillatory Field,&quot;

Verification of Nozzle Admittance Theory by Exact Measurement of the Admittance Parameter,&quot;

http://authors.library.caltech.edu/22034/1/359_Cukick_FEC_1993.pdf

Oscillatory and unsteady processes in liquid rocket engines

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Caltech Authors - Main