Reports and Technical Reports
An investigation of the effect of acceleration on the burning rate of composite propellants
(Monterey, California. Naval Postgraduate School, 1967-07-28); NPS-57RV7071A
The average burning rates of composite solid rocket propellant were measured in acceleration
fields up to 2000 times the standard acceleration of gravity. The acceleration vector was
perpendicular to and into the burning ...
Temperature Distributions in Thin Circular Disks with Variable Thickness, Thermal Conductivity, and Heat Transfer Coefficient (A Direct Variational Approach using Rayleigh Ritz Approximation)
(Monterey, California. Naval Postgraduate School, 1966); Technical Note No. 66T-5
An approximate solution for the temperature distribution
in a thin circular disk having variable thermal properties,
variable thickness, and a variable surface heat transfer coefficient
is presented. The method used was ...
Radial-Inflow Turbines
(Monterey, California. Naval Postgraduate School, 1964-04); 64T-4
Range of Orifice Measurements for Mapping of Allis-Chalmers Axial-Flow Compressor
(Monterey, California. Naval Postgraduate School, 1963-08); TN No. 63T-3
An Investigation of the Flow Conditions at the Lower Measuring Plane, and in the Plenum Chamber of the Rectilinear Cascade Test Facility
(Monterey, California. Naval Postgraduate School, 1966-04); Technical Report No. 66T-3
This report describes the tests made to determine the flow
conditions that exist ahead of the cascade and establishes a basis
for future modification of the cascade test facility. The investigation
was conducted with ...
Electric Drive for CIT Axial-Flow Test Blower
(Monterey, California. Naval Postgraduate School, 1964); Technical Note No. 64T-2
Determination of the Momentum Drag within the Turbojet Engine Laboratory While Operating the J-57-8B Turbojet Engine
(Monterey, California. Naval Postgraduate School, 1964-09); Technical Note No. 64T-6
Limited tests were conducted at the USNPGS Astro /Aeronautical Propulsion
Laboratories to determine the magnitude and variation of the momentum
drag which is developed within turboject engine test chamber
while operating ...
Determination of Flow Rates Transonic Turbine Test Rig
(Monterey, California. Naval Postgraduate School, 1966-01); Technical Note No. 66T-1
Determination of Flow Rates of Allis-Chalmers Axial Flow Compressor VA-312 of Propulsion Laboratories by Means of Square-Edged Orifices
(Monterey, California. Naval Postgraduate School, 1963-08); Technical Note No. 63T-2
Data Reduction for the Compressor Test Rig
(Monterey, California. Naval Postgraduate School, 1964-01); Technical Note No. 64T-1
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Aeronautics (15)