Results 191 to 200 of about 385,605 (249)

Analysis of Mach number 0.8 turboprop slipstream wing/nacelle interactions

H. Robert Welge, Dan Neuhart, J. A. Dahlin   +2 more
openalex   +1 more source

3D conformation and crystal interaction insights into drug development challenges for HCV drug analogues via molecular simulations. [PDF]

Commun Chem
Hong RS, Mattei A, Tuckerman ME, Sheikh AY.   +3 more
europepmc   +1 more source

The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

, 1952
I. E. Beckwith, Herbert W Ridyard, Nancy Cromer   +2 more
openalex   +1 more source

Aerodynamic investigation of a parabolic body of revolution at mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base

, 1956
Eugene S Love
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Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured in Flight on the Wing of the D-558-I Research Airplane Through a Mach Number Range of 0.80 to 0.89 and Throughout the Normal-force-coefficient Range at Mach Numbers of 0.61, 0.7

, 1951
E. R. Keener, Rozalia M Bandish
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Development and Comparative Analysis of an AI Based Convolutional Neural Network Algorithm versus Dentists of Varying Experience in Detecting Dental Caries using Bitewing X-ray Images: An <i>In vitro</i> Study.

J Pharm Bioallied Sci
Albadr AK.
europepmc   +1 more source

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Detonation Wave Mach Number Dependence in a High Mach Number Flows

22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018
The paper presents a study of detonation propagation in supersonic crossflows over a range of Mach numbers. The work is focused on characterizing the detonation wave dependence on the supersonic cross-stream Mach number. A high-enthalpy combustor is used to provide continuous premixed supersonic crossflows that interact with an orthogonal detonation ...
Sosa, Jonathan, Rosato, Daniel, Ahmed, Kareem A.   +2 more
openaire   +2 more sources