Longitudinal trim, Other Engineering

Assignment Help:

A trimmed flight condition is perhaps best thought of as an equilibrium condition. The simplest trim condition is straight-and-level flight, in which the forces (weight, propulsive, aerodynamic) balance and the moments (aerodynamic and propulsive) sum to zero3.

In this particular trim, the accelerations and angular accelerations are all zero. An aircraft could also be trimmed in a steady banked level turn, a climb, a powered descent, though note that (for example) in a steady turn, the forces and moments will not be balanced because a resultant force and a resultant moment are required to provide the necessary centripetal acceleration (rate-of-change of momentum) and the necessary precession of the angular momentum vector (rate-of-change of angular momentum). 


Related Discussions:- Longitudinal trim

Common faults - fire safety management, Common faults - Fire safety managem...

Common faults - Fire safety management: Common faults found are: Combustible items left in protected routes Locked exits Fire doors wedged open Exits obstru

Pitot intakes - aircraft maintenance , Pitot intakes: This intake is su...

Pitot intakes: This intake is suitable for subsonic or low supersonic speeds. Examples, 707, 747, A300B, Tristar, etc. The intake is usually short and is very efficient becau

Fibre optics communications, explain the fibre optic communication system w...

explain the fibre optic communication system with block diagram

Business Management Techniques -Company organisation, Business functions of...

Business functions of engineering firm 2.1-Engineering business: 2.2- Functions of engineering business

Assignment , I want help for the circuit theory

I want help for the circuit theory

Biology, Any Biology Modeling software?

Any Biology Modeling software?

Elecrical communication, explain application of zener diode for meter prote...

explain application of zener diode for meter protection

Control surfaces , Control Surfaces  As with a flight control system...

Control Surfaces  As with a flight control system, a guidance algorithm uses control surfaces to control the behaviour of an airframe.         - Rudder, ailerons, elev

Basic electronics, Q 1.what is the difference between BJT and FET.What is B...

Q 1.what is the difference between BJT and FET.What is Biasing?Discuss abt diffrent Biasing techniques?Write the advantages and Volatage divider biasing over other biasing?what is

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd