A method for determining the thrust of an aircraft engine, based on information available from tracking the aircraft air-speed, acceleration, and position, the method comprising calculating the thrust, using the equation Thrust = mgH'/V + mV' + Drag, where m is the aircraft estimated mass, ...
Open Aircraft Performance Model and Python Toolkit dragfuelaircraftthrustaircraft-performance UpdatedDec 26, 2024 Python Header only framework for data analysis in massively parallel platforms. openmpparallel-computingcudaparallelizationhydraheader-onlydata-analysismonte-carlo-simulationparallel-algorithmhigh-energy...
which include the improvement of low-observability (LO) as well as the reduction of aircraft mass and zero-lift dragCW0. This can result in higher specific thrust and increased range or payload [2]. Thus, this technology can
[15] investigated the impact of engine architecture and installation position on the aerodynamic behaviour of a wide-body 300-seater aircraft using RANS CFD. A parametric geometry definition based on intuitive Class-Shape Transformation functions (iCSTs) [31] was employed for the design of the ...
Time-optimal reorientation maneuvers for an aircraft with thrust-vector control - Navigation and Control Conference (AIAA) thrust-vector control system AIAA 被引量: 3发表: 2000年 THRUST VECTOR CONTROL PROBLEM TO BE SOLVED: To lighten and miniaturize a whole device which controls the thrust vector ...
Analysis of control system responses for aircraft stability and efficient numerical techniques for real-time simulations The engine power dynamic response was modeled with an additional state equation as first order lag in the actual power level response to commanded power level was computed as a funct...
The clam doors, which form an integral part of the tailpipe, open when the system is deployed and duct the exhaust gases around so that they flow forward to oppose the forward movement of the aircraft. An Illustrated Dictionary of Aviation Copyright © 2005 by The McGraw-Hill Companies, ...
BL Nagabhushan,SB Tan - 《Journal of Aircraft》 被引量: 26发表: 1995年 Closed electron drift plasma thrustor with orientable thrust vector the device includes several annular channels on a platinum core ionization and acceleration (124a, 124b) having non parallel axes (241a, 241b) which co...
One dynamic thrust plot is shown below, comparing actual, measured values to calculated results from my equation above: For more details, more in-depth explanations, and additional figures, see the article at its original posting location here:http://electricrcaircraftguy.blogspot.com/2013/09/prop...
To improve the performance of the motor, theoretical equation is required for mathematical analysis. In this paper, a relation between the motor performance and structural parameter is clarified by solving the thrust equation of the motor. By comparing calculation result based on the......