نتایج جستجو برای: southwest oriented thrust

تعداد نتایج: 155326  

Journal: :JACEP 1976
C W Guildner D Williams T Subitch

To investigate the application of a cough-creating thrust for the removal of airway-obstructing foreign material, the thrust was applied to six adult male anesthetized volunteers at the waist, at the low chest level, and at the midchest level, with the subjects in both the horizontal-lateral and the sitting positions. Air volume, peak air flow rate, and airway measurements were made. Both the l...

Journal: :Earth-Science Reviews 2022

Both the kinematics and dynamics of topographic growth Tibetan Plateau remain debated, despite their significance for understanding evolution continental lithospheric geodynamics, climate, biodiversity in Asia. Topographic swath profiles reveal diversity high-elevation, low-relief plateau surfaces or “relict landscapes” throughout southeast Qiangtang, northeast Songpan-Garze-Yidun terranes east...

2014
Yujing SONG Ming ZHANG Yu ZHU

Wherein, the thrust fluctuation is an important factor affecting the positioning accuracy of the workpiece table. Many scholars have studied the thrust fluctuation reduction methods to improve the motor performance. Some articles optimized structure size [1], or the analytical method ignoring the end effect [2], or using look-up tables [3]. Another scholars have adopted active control strategy ...

Journal: :CoRR 2017
Namrata Gupta Mangal Kothari Abhishek

This paper carries out the mathematical modeling, simulation, and control law design for a quadrotor with variable-pitch propellers. The use of variable-pitch propeller for thrust variation instead of RPM regulation facilitates generation of negative thrust, thereby augmenting the rate of change of thrust generation amenable for aggressive maneuvering. Blade element theory along with momentum t...

2013
Xin H. Zou Qiang Wang

The comparisons of two typical fluidic thrust vectoring exhaust nozzles including two-dimensional(2-D) nozzle and axisymmetric nozzle on aerodynamic characteristics was presented by numerical simulation. The results show: the thrust vector angles increased with the increasing secondary flow but decreased with the nozzle pressure ratio (NPR) increasing. With the same secondary flow and NPR, the ...

2009
Ufuk Topcu Jordi Casoliva

Motivated by the requirement for pinpoint landing in futureMarsmissions, we consider the problemofminimumfuel powered terminal descent to a prescribed landing site. The first-order necessary conditions are derived and interpreted for a point-mass model with throttle and thrust angle control and for rigid-bodymodel with throttle and angular velocity control, clarifying the characteristics of the...

Journal: :journal of sciences islamic republic of iran 0

average values of< 1- t >where t is the thrust are presented for e: e: amy data and are compared with their values in hadronic interactions. as far as possible, similar analysis techniques have been employed in the two different interactions. similar variation with e is observed for this average in both data. the values of < pt> and < pl > relative to the thrust axis in e e are similar to those...

Journal: :geopersia 2012
hossein narimani ali yassaghi mohammad-ghasem hasan-goodarzi

allochthonous masses are common structures in zagros fold-thrust belt. they are generally considered as collapse structures formed by the influence of gravity and in rock units with competency contrast. however, large allochthonous masses mapped in dowgonbadan area in dezful embayment near the mountain front fault (mff) of zagros show characteristics different from the belt common collapse stru...

2002
Alexander G. Webb Julien Célérier T. Mark Harrison Olivier Beyssac Frédéric Herman William J. Dunlap

An integrated petrologic, thermochronologic, and numerical modeling study constrains the thermal evolution of the Lesser Himalayan Sequence in the Kumaun and Garwhal regions of India. South of the Tons thrust, peak metamorphic temperatures do not exceed 330 °C. On the northern side, a transition toward higher temperatures adjacent to the Main Central thrust hanging wall is documented. In the im...

2004
Jorge Delgado Michael M. Micci Benjamin Welander

A low-power microwave arjet thruster was studied using ammonia gas as propellant. The purpose of the project was to generate ammonia plasma using a 7.5 GHz magnetron and a cylindrical cavity thruster, which is resonant in the TM001 mode [1]. The desired pressure was atmospheric or above while generating a thrust of roughly 20mN and an Isp of about 500s operating at low power (<100 kW). Introduc...

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