Subsonic aircraft's unsteady longitudinal stability derivatives calculation

zbMATH Open1002.76055MaRDI QIDQ2774621

Nikola Maričić

Publication date: 26 February 2002

zbMATH Keywords

aerodynamic coefficientsdoublet lattice methodaerodynamics fluttercanard wingsoftware DERIVsubsonic aircrafttransport plane wingunsteady longitudinal aerodynamics stabilitywing HA21Awing HA75H

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Particle methods and lattice-gas methods (76M28) Hydrodynamic stability (76E99)

Related Items (4)

Approximate solutions of range for constant altitude – constant high subsonic speed flight of transport aircraft ⋮ Decoupling of the longitudinal modes of advanced aircraft ⋮ Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation ⋮ Title not available (Why is that?)

Uses Software

• NASTRAN

Recommendations

• Lifting surface in subsonic unsteady regime 👍 👎
• Asymptotic analysis of aircraft wing model in subsonic airflow 👍 👎
• Asymptotic analysis of aircraft wing model in subsonic air flow. 👍 👎
• Numerical determination of dynamic derivatives for transport aircraft 👍 👎
• Numerical estimation of aircrafts' unsteady lateral-directional stability derivatives 👍 👎
• Software development for subsonic aircraft’s unsteady longitudinal stability derivatives calculation 👍 👎
• Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds 👍 👎
• Title not available (Why is that?) 👍 👎
• Title not available (Why is that?) 👍 👎
• Title not available (Why is that?) 👍 👎

This page was built for publication: Subsonic aircraft's unsteady longitudinal stability derivatives calculation

Report a bug (only for logged in users!)Click here to report a bug for this page (MaRDI item Q2774621)