Term
|
Definition
| is a quantity that represents only magnitude |
|
|
Term
|
Definition
| is a quanitity that represents both magnitude and direction |
|
|
Term
|
Definition
| is a push or pull exerted on a body |
|
|
Term
|
Definition
| is the quantity of molecular material that comprises an object |
|
|
Term
|
Definition
| amount of space occupied by an object |
|
|
Term
|
Definition
| force with which a mass is attracted toward the center of the earth by gravity |
|
|
Term
|
Definition
|
|
Term
|
Definition
| a vector quantity equal to a force F * s (distance) |
|
|
Term
|
Definition
| rate of doin work or work done per unit time P= w/t |
|
|
Term
|
Definition
| a scalar measure of body's capacity to do work |
|
|
Term
|
Definition
| ability of a body to do work because of its position or state of being |
|
|
Term
|
Definition
| ability of a body to do work because of its motion |
|
|
Term
| eqquilibrium flight exists when... |
|
Definition
| the sum of all forces AND the sum of all moments around the COG are equal to zero |
|
|
Term
| Trimmed flight exists when... |
|
Definition
| the sum of all moments around the COG is equal to zero |
|
|
Term
|
Definition
| A body at rest tends to remain at rest and a body in motino tends to remain in a straight line at a constant velocity unless acted upon by some unbalanced force |
|
|
Term
|
Definition
unbalanced force acting ona body produces an acceleration in the direction of the force that is directly proportional to the force and inversely proportional to themass of the body (F = m * a) |
|
|
Term
|
Definition
| For every action there is an equal and opposite reaction |
|
|
Term
|
Definition
| the pressure particles of air exert on adjacent bodies |
|
|
Term
| ambient static pressure is |
|
Definition
| equal to the weight of a column of air over a given area |
|
|
Term
|
Definition
| is the total mass of air particles per unit of volume |
|
|
Term
|
Definition
| is a measure of Average Random Kinetic Energy |
|
|
Term
| Air density (increases/decreases) with an increase in altitude |
|
Definition
|
|
Term
| Rate of T change (avg lapse rate) is |
|
Definition
| 2 deg Cel/ 3.57 deg F per 1000 feet until 36000 feet. |
|
|
Term
|
Definition
| amount of water vapor in the air |
|
|
Term
| as humidity increases, density... |
|
Definition
|
|
Term
|
Definition
| measure of air's resistance to flow and shearing |
|
|
Term
| air viscosity increases with an (increase/decrease) in temp? |
|
Definition
|
|
Term
|
Definition
|
|
Term
Local speed of sound is ... dependent on... |
|
Definition
| rate at which sound travels through an air mass..... dependent on TEMPERATURE |
|
|
Term
| Standard atmosphere (engineering baseline) |
|
Definition
| a set of reference conditions giving representative values of air properties as a function of altitude |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| 3.57 deg F 2 deg C per 1000 ft |
|
|
Term
| local speed of sound UNITS |
|
Definition
|
|
Term
|
Definition
| height above the standard datum plane |
|
|
Term
|
Definition
| actual height above mean sea level |
|
|
Term
|
Definition
| is the altitude in standard atmosphere where the air density is equal to local air density |
|
|
Term
|
Definition
| any device used for flight in air |
|
|
Term
|
Definition
heaveier than air fixed wing engine driven supported by the dynamic reaction of airflow over wings |
|
|
Term
|
Definition
| basic structure of the airplane to which all other compnents are attached |
|
|
Term
|
Definition
| type consists of metal or wooden frame of which a light skin is stretched |
|
|
Term
|
Definition
| extremely light consisists of only a skin shell (easily damaged) |
|
|
Term
|
Definition
| support from skin and frame T34! |
|
|
Term
|
Definition
| airfoil attached to the fuselage designed to produce lift |
|
|
Term
| T34 all bracings are internal so wings are considered... |
|
Definition
|
|
Term
|
Definition
| aft part of fuselage, vertical stabilizer, horizontal stabilizer |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| point at which all weight is concentrated about and all forces and moments measured from |
|
|
Term
|
Definition
|
|
Term
|
Definition
b * c (wingspan) * (average chord) |
|
|
Term
|
Definition
| reduction in the chord of an airfoil from root to tip |
|
|
Term
|
Definition
| angle between airplanes longitudinal axis and chordline of the wing |
|
|
Term
|
Definition
|
|
Term
| dihedral is angle between |
|
Definition
| spancewise inclination and lateral axis |
|
|