In Flight Negative Pion Assessments Using Time-of-Flight Technique
نویسندگان
چکیده
منابع مشابه
Time of Flight Technique
At first glance, the traditional Time of Flight (TOF) technique for identification of pions, kaons and protons seems to be ideally suited for the momentum range of particles produced at the Tau-Charm Factory. In the decays of r leptons and charmed mesons most of the secondaries have momentum smaller then 1 GeV/c. The exception are the twoand three-body decays of $J and $’ where the region of in...
متن کاملTime-of-flight estimation using binary search system identification technique
( ) ( ) ( ) t gs D t r t s + − = , (1b) where the x(t) consists of a reference signal r(t), and Gaussian noise gx(t), while the s(t) consists of the time delayed version of the reference signal r(t-D), and Gaussian noise gs(t). Additionally let us assume that the noise signals are uncorrelated with each other and with the reference signal. The TOF lies at the core of many modern signalprocessin...
متن کاملFlight Simulation: Research Challenges and Flight Crew Assessments of Fidelity
The principal aim of simulation is to provide a platform on which environments or technology, either real or proposed, may be recreated for the purposes of training, visualisation and research. Simulators’ fidelity range widely; some aim to recreate an environment or system to such a high degree that it is difficult to distinguish between the simulator and the real system, while others simply a...
متن کاملHelicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight
An implicit unsteady upwind solver including a mesh motion approach was applied to simulate a helicopter including body, main rotor and tail rotor in hover flight. The discretization was based on a second order finite volume approach with fluxes given by the Roeand#39;s scheme. Discretization of Geometric Conservation Laws (GCL) was devised in such a way that the three-dimensional flows on arbi...
متن کاملStress Analysis of Flight Vehicles under Flight Conditions
A method is presented for the stress analysis of flight vehicles under different flight conditions including gust and control surface deflection (or maneuver) using the governing equations of rigid-body motions and elastic deformations. The Lagrangian approach is used to derive the governing equations of motions. For this purpose, the basic equations of motions are derived in terms of potential...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of UOEH
سال: 1984
ISSN: 0387-821X,2187-2864
DOI: 10.7888/juoeh.6.57