781 results on '"Moore, R. D."'
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102. Gonorrhoea and chlamydia testing rates of HIV-infected men: low despite guidelines
103. Hepatitis C seropositivity is not a risk factor for sensory neuropathy among patients with HIV
104. Correction to “Detection of runoff timing changes in pluvial, nival, and glacial rivers of western Canada”
105. Detection of runoff timing changes in pluvial, nival, and glacial rivers of western Canada
106. Excess mortality after HIV seroconversion has greatly decreased in the past 10 years
107. Introduction to the Special Issue on Recent Advances in Canadian Hydrology, 2003-2007
108. Glacier change in western North America: influences on hydrology, geomorphic hazards and water quality
109. Advances in Canadian Forest Hydrology, 2003-2007
110. Supersonic throughflow fans
111. Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
112. Comparison of analytical and experimental performance of a wind-tunnel diffuser section
113. Wind tunnel turning vanes of modern design
114. Wind tunnel turning vanes of modern design
115. Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage
116. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05
117. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82
118. Aerodynamic performance of 0.4066-scale model to JT8D refan stage
119. Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 deg
120. Aerodynamic Performance of Two Variable-Pitch Fan Stages
121. Performance of a low-pressure fan stage with reverse flow
122. Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor
123. Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage
124. Prediction of pump cavitation performance
125. Performance of transonic fan stage with weight flow per unit annulus area of 178 kilograms per second per square meter (6.5(lb/sec)/(sq ft))
126. Performance of transonic fan stage with weight flow per unit annulus area of 198 kilograms per second per square meter (40.6(lb/sec)/sq ft)
127. Performance of a single-stage transonic compressor with a blade-tip solidity of 1.5 and comparison with 1.3 and 1.7 solidity stages
128. Performance of transonic fan stage with weight flow per unit annulus area of 208 kilograms per second per square meter (42.6 (lb/sec)/sq ft)
129. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26 respectively, and with design pressure ratio of 2.05
130. Experimental study of low aspect ratio compressor blading
131. Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles
132. Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage
133. Experimental study of low aspect ratio compressor blading
134. Vertical Takeoff and Landing (VTOL) propulsion technology
135. Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 1.82
136. Performance of a transonic fan stage designed for a low meridional velocity ratio
137. Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage
138. Design and overall performance of four highly loaded, high speed inlet stages for an advanced high-pressure-ratio core compressor
139. Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet
140. Performance of low-pressure-ratio fan stage at two off-design blade setting angles
141. Effect of casing treatment of overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5
142. Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment
143. Performance of 1.15-pressure-ratio fan stage at several rotor blade setting angles with reverse flow
144. Aerodynamic performance of a 1.20-pressure ratio fan stage designed for low noise
145. Implementing the Amphibian Conservation Action Plan
146. Cohort profile: the Centers for AIDS Research Network of Integrated Clinical Systems
147. Coupled modelling of glacier and streamflow response to future climate scenarios
148. Survival during Renal Replacement Therapy among African Americans Infected with HIV Type 1 in Urban Baltimore, Maryland
149. Immune Status at Presentation to Care Did Not Improve among Antiretroviral-Naive Persons from 1990 to 2006
150. CD4+ Cell Count 6 Years after Commencement of Highly Active Antiretroviral Therapy in Persons with Sustained Virologic Suppression
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