REVISTA

Aerospace

ISSN: 2226-4310 Frecuencia: 4 Formato: Electrónica

Tablas de contenido

17 artículos asociados

Volumen 3 Número 0 Parte 4 Año 2016

Correction: Iemma, U. Theoretical and Numerical Modeling of Acoustic Metamaterials for Aeroacoustic Applications. Aerospace 2016, 3, 15	Acceso
Umberto Iemma

A Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows, Part Two: Multi-Dimensional Analysis	Acceso
Vincent Casseau, Daniel E. R. Espinoza, Thomas J. Scanlon and Richard E. Brown

Continuation Methods for Nonlinear Flutter	Acceso
Edward E. Meyer

Gaskinetic Modeling on Dilute Gaseous Plume Impingement Flows	Acceso
Chunpei Cai

Analysis of Pilot-Induced-Oscillation and Pilot Vehicle System Stability Using UAS Flight Experiments	Acceso
Tanmay K. Mandal and Yu Gu

On the Importance of Morphing Deformation Scheduling for Actuation Force and Energy	Acceso
Roeland De Breuker and Noud Werter

Recent Advances in Aeroacoustics	Acceso
Luís M. B. C. Campos

Effect of Leading-Edge Slats at Low Reynolds Numbers	Acceso
Lance W. Traub and Mashaan P. Kaula

Climate-Compatible Air Transport System?Climate Impact Mitigation Potential for Actual and Future Aircraft	Acceso
Katrin Dahlmann, Alexander Koch, Florian Linke, Benjamin Lührs, Volker Grewe, Tom Otten, Doreen Seider, Volker Gollnick and Ulrich Schumann

Results of Long-Duration Simulation of Distant Retrograde Orbits	Acceso
Gary Turner

Wing Tip Drag Reduction at Nominal Take-Off Mach Number: An Approach to Local Active Flow Control with a Highly Robust Actuator System	Acceso
Matthias Bauer, Thomas Grund, Wolfgang Nitsche and Vlad Ciobaca

Numerical Investigation of Effect of Parameters on Hovering Efficiency of an Annular Lift Fan Aircraft	Acceso
Yun Jiang and Bo Zhang

A Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows, Part One: Zero-Dimensional Analysis	Acceso
Vincent Casseau, Rodrigo C. Palharini, Thomas J. Scanlon and Richard E. Brown

Linearized Euler Equations for the Determination of Scattering Matrices for Orifice and Perforated Plate Configurations in the High Mach Number Regime	Acceso
Moritz Schulze, Michael Wagner and Thomas Sattelmayer

An Empirical Study of Overlapping Rotor Interference for a Small Unmanned Aircraft Propulsion System	Acceso
Mantas Brazinskas, Stephen D. Prior and James P. Scanlan

Comparison of Power Requirements: Flapping vs. Fixed Wing Vehicles	Acceso
Gottfried Sachs

Numerical Study of Transition of an Annular Lift Fan Aircraft	Acceso
Yun Jiang and Bo Zhang