Solid Propellant Combustion Diagnostics and Automated Data Retrieval from Holograms, (9999)
Glenn,J. M., Graham,K. J., Harris,R. K., Lee,Y., Netzer,D. W.
High speed motion pictures, holography and measurements of scattered laser light are being used to study the behavior of particulate matter in the combustion products in solid rocket propellants. An...
Naval Postgraduate School (2007)
Monterey California Approved, Radm Robert, C. Chaplin, R. Elster, Cynthia E. Irvine, Cynthia E. Irvine, ...
Maximum 200 words.) It is anticipated that the introduction of metacomputing and distributed resource management mechanisms to the Internet and World Wide Web will make available to users and...
An analytical method is presented for determining the flow characteristics of a two-phase flow of liquid drops in a gas stream as the mixture expands through an annular converging-diverging nozzle....
An Experimental Investigation of the Dual Chamber Rocket, (2002)
An experimental investigation was conducted to determine the feasibility and practicality of the dual chamber rocket concept. Cold flow studies were performed which utilized a telescoping booster...
An Experimental Investigation of the Dual Chamber Rocket Motor. (2002)
Van Brocklin,S. T., Beakley,J. E., Netzer,D. W.
An experimental investigation was conducted to further determine the operating characteristics of the dual chamber rocket motor. Axisymmetric and two-dimensional apparatuses were used with air flow...
Initial Validation of an Ambient Air Quality Model for Naval Air Operations. (2002)
A previously developed model was updated to appropriately represent 1978/79 operations and then evaluated for prediction sensitivity to variations in meteorological and dispersion model parameters. A...
Gas Turbine Combustor and Engine Augmentor Tube Sooting Characteristics. (2002)
Bennett,J. S., Jway,C. H., Urich,D. J., Netzer,D. W.
An experimental investigation was conducted to investigate the effects of smoke-suppressant fuel additives, fuel composition and combustor operating environment on the soot characteristics within the...
Data Integrity Limitations in Hybrid Security Architectures (2000)
Radm Admiral, David R. Ellison, R. Elster, Cynthia Irvine, Cynthia E. Irvine, Timothy Levin, ...
Maximum 200 words.) We discuss a class of computer/network architectures that supports multilevel security and commercial applications, while utilizing primarily commercial-off-the-shelf (COTS)...
Nonmetallized Composite Propellant Combustion. (1998)
Netzer,D. W., Kennedy,J. R., Brown,W. E.
An experimental investigation of nonmetallized composite propellant combustion in standard and high acceleration environments was made. Pressed ammonium perchlorate (AP) pellets of varying purity,...
Ammonium Perchlorate and Ammonium Perchlorate - Binder Sandwich Combustion. (1998)
Single crystal and pressed polycrystalline ammonium perchlorate (AP) wafers, pressed polycrystalline AP pellets, and ammonium perchlorate-binder (polybutadiene acrylic acid, hydroxyl terminated...
Klahr,O. A., Gerhardt,R. R., Netzer,D. W.
Nonmetallized double-base and composite propellant, metallized composite propellant, and ammonium perchlorate (AP)/binder sandwich combustion were studied in standard and high acceleration...
PARAMETRIC STUDY OF ROCKET INSTABILITY. (1998)
The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating...
INVESTIGATION OF COMBUSTION CHARACTERISTICS OF A BI-PHASE ROCKET, (1998)
An investigation was conducted (a) to test the ability of the Priem-Heidmann propellant vaporization model to predict the steady-state operating characteristics of a bi-phase rocket motor, (b) to...
Three-Dimensional, Primitive-Variable Model for Solid-Fuel Ramjet Combustion. (1998)
A three-dimensional computer code has been developed for the solid-fuel ramjet combustion process. The code includes finite-rate chemical kinetics and has been used to predict the combustion behavior...
Measurements of Gas Turbine Combustor and Engine Augmentor Tube Sooting Characteristics. (1998)
Young, M. F., Grafton, T. A., Conner, H., Netzer, D. W.
An experimental investigation was conducted to determine the changes in soot mean diameter across the combustor and exhaust nozzle of a T63 gas turbine engine, and across an exhaust augmentor tube....
Measurements of gas turbine combustor and engine augmentor tube sooting characteristics.
Grafton, Thomas A. III., Netzer, D.W.
Thesis advisor, D.W. Netzer.