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Catégorie :Category: nCreator TI-Nspire
Auteur Author: centsz
Type : Classeur 3.0.1
Page(s) : 1
Taille Size: 1.46 Ko KB
Mis en ligne Uploaded: 17/12/2024 - 03:48:49
Mis à jour Updated: 17/12/2024 - 03:50:12
Uploadeur Uploader: centsz (Profil)
Téléchargements Downloads: 2
Visibilité Visibility: Archive publique
Shortlink : http://ti-pla.net/a4413065
Type : Classeur 3.0.1
Page(s) : 1
Taille Size: 1.46 Ko KB
Mis en ligne Uploaded: 17/12/2024 - 03:48:49
Mis à jour Updated: 17/12/2024 - 03:50:12
Uploadeur Uploader: centsz (Profil)
Téléchargements Downloads: 2
Visibilité Visibility: Archive publique
Shortlink : http://ti-pla.net/a4413065
Description
Fichier Nspire généré sur TI-Planet.org.
Compatible OS 3.0 et ultérieurs.
<<
uniform circular motion: Ac = v^2/r a= v / t Fc = mv^2/r V = 2piR / T Ac = 4pi^2r/ T^2 T= time/ # of cycles Tension in uniform circular motion: Left and right: T = mv^2/r Top = mv^2/r -mg Bottom: T =mv^2/r +mg Horizantal circle: no angle: T = mv^2/r with angle: T= sqrt(tx^2 +ty^2) Centripetal Acceleration: ac = F/m ac = v^2/r Time period: 2pir / t Speed with period: 4pi^2r/ t^2 speed of sateleite: v = sqrt(Gm/R) R = (height of satelite in m) + (radius of planet) Time period for satelite: T = 2piR / V (in seconds) height of satelite above surface of earth = R= 3rdroot(GmT^2/4pi^2) Time period of Satelite: T= 2pi* sqrt(r^3/Gm) Gravitational field formula: GM/r^2 Made with nCreator - tiplanet.org
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Compatible OS 3.0 et ultérieurs.
<<
uniform circular motion: Ac = v^2/r a= v / t Fc = mv^2/r V = 2piR / T Ac = 4pi^2r/ T^2 T= time/ # of cycles Tension in uniform circular motion: Left and right: T = mv^2/r Top = mv^2/r -mg Bottom: T =mv^2/r +mg Horizantal circle: no angle: T = mv^2/r with angle: T= sqrt(tx^2 +ty^2) Centripetal Acceleration: ac = F/m ac = v^2/r Time period: 2pir / t Speed with period: 4pi^2r/ t^2 speed of sateleite: v = sqrt(Gm/R) R = (height of satelite in m) + (radius of planet) Time period for satelite: T = 2piR / V (in seconds) height of satelite above surface of earth = R= 3rdroot(GmT^2/4pi^2) Time period of Satelite: T= 2pi* sqrt(r^3/Gm) Gravitational field formula: GM/r^2 Made with nCreator - tiplanet.org
>>
