Примери коришћења Dihedral на Енглеском и њихови преводи на Српски
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The first dihedral is good.
The vertical location of the CG changes the amount of dihedral effect.
The purpose of dihedral effect is to contribute to stability in the roll axis.
Wing sweepback also increases dihedral effect.
Dihedral effect is defined simply to be the rolling moment caused by sideslip and nothing else.
Other factors contributing to dihedral effect.
Its typical dihedral angles(-75°, 160°) are close, but not identical to, those of the PPII helix.
The CG of a paraglider is very low,making a strong contribution to dihedral effect.
For comparison, the sum of the dihedral angles for an α-helix is roughly- 105°, whereas that for a π-helix is roughly- 125°.
Disulfides show a distinct preference for dihedral angles approaching 90°.
For comparison, the sum of the dihedral angles for a 310 helix is roughly- 75°, whereas that for the π-helix is roughly- 130°.
An extreme example of the effect of vertical CG on dihedral effect is a paraglider.
The dihedral or torsional terms typically have multiple minima and thus cannot be modeled as harmonic oscillators, though their specific functional form varies with the implementation.
Ideally, the tip of the soldering iron should be dihedral with an angle of at least 30°.
Since dihedral effect is noticed by pilots when"rudder is applied", many pilots and other near-experts explain that the rolling moment is caused by one wing moving more quickly through the air and one wing less quickly.
Indeed, these are actual effects, butthey are not the dihedral effect, which is caused by being at a sideslip angle, not by getting to one.
NMR and FRET methods can be used to determine complementary information including relative distances, dihedral angles, angles, and connectivity.
Roll stability is less-ambiguously termed"spiral mode stability" and dihedral effect is a contributing factor to it, but dihedral effect is not any kind of stability by itself.
This class of terms may include improper dihedral terms, which function as correction factors for out-of-plane deviations(for example, they can be used to keep benzene rings planar, or correct geometry and chirality of tetrahedral atoms in a united-atom representation).
Military fighter aircraft often have near zero oreven anhedral angle reducing dihedral effect and hence reducing the stability of the spiral mode.
The twist is often associated with alternating fluctuations in the dihedral angles to prevent the individual β strands in a larger sheet from splaying apart.
During design of a fixed-wing aircraft(or any aircraft with horizontal surfaces),changing dihedral angle is usually a relatively simple way to adjust the overall dihedral effect.
This difference in lift between the wings is a rolling moment, and since it is caused by sideslip,it is dihedral effect(or more correctly, it is a contribution to the total dihedral effect of the aircraft).
Unlike the alpha helix and beta sheet,the alpha sheet configuration does not require all component amino acid residues to lie within a single region of dihedral angles; instead, the alpha sheet contains residues of alternating dihedrals in the traditional right-handed(αR) and left-handed(αL) helical regions of Ramachandran space.