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...

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...

The thrust and plasma parameters generated by a Helicon Double Layer Thruster operating at a power level of 250 W with krypton propellant has been evaluated for peak magnetic field strengths of 0 to 270 G. Results show that the thrust levels achieved are dependent on the position of peak magnetic field in relation to the plasma source. Alignment of peak field strength with the plasma source exi...

A retargeting procedure is developed for use as a nonlinear low thrust guidance scheme. The selection of a control program composed of a sequence of inertially fixed thrust-acceleration vectors permits all trajectory computations to be made with closed form expressions, and allows the controls to be represented by constant parameters, thrust-acceleration vectors and thrusting times. By requirin...

During preliminary aircraft design, the vertical tail sizing is conventionally conducted by use of volume coefficients. These represent a statistical approach using existing configurations’ correlating parameters, such as wing span and lever arm, to size empennage. For more detailed analysis with regard control performance, strongly depends on critical loss thrust assessment. This consideration...

Based on the bionic design of humpback whale fin, a passive flow control method is proposed to obtain greater flapping lift by applying wavy leading edge structure straight symmetrical wing. The conventional wing replaced shape represented regular trigonometric function form special configuration imitating fin. dynamic aerodynamic performance and field characteristics with different parameters ...

Speed and position control systems for marine vehicles have been subject to an increased focus with respect to performance and safety. An example is represented by drilling operations performed with semi submersible rigs where the control of position and heading requires high accuracy. Drifting from the well position could cause severe damage to equipment and environment. Also, the use of under...

Sandbox experiments with different boundary conditions demonstrate that antiformal stacks result from a forward-breaking thrust sequence. An obstacle blocks forward thrust propagation and transfers the deformation back to the hinterland in a previously formed true duplex. In the hinterland, continued shortening causes faults to merge toward the tectonic transport direction until the older thrus...

UAVs are designed to create lift in the same direction as rotation axis, hence propellers one of most basic components propulsion. Although several previous propeller optimization techniques have been developed, they usually find optimal thrust coefficient at a constant power and vice versa. This research will combine values optimum lowest time. A Simple Blade Element Theory served foundation f...

The aims of this study were to explore the hydrodynamic mechanism of Xenopus laevis swimming and to describe how hind limb kinematics shift to control swimming performance. Kinematics of the joints, feet and body were obtained from high speed video of X. laevis frogs (N=4) during swimming over a range of speeds. A blade element approach was used to estimate thrust produced by both translational...