REVISTA

Aerospace

ISSN: 2226-4310 Frecuencia: 4 Formato: Electr�nica

Tablas de contenido

30 art�culos asociados

Volumen 5 N�mero 1 Parte March A�o 2018

Buoyancy-Induced Heat Transfer inside Compressor Rotors: Overview of Theoretical Models	Acceso
J. Michael Owen, Hui Tang and Gary D. Lock

CFD Validation and Flow Control of RAE-M2129 S-Duct Diffuser Using CREATETM-AV Kestrel Simulation Tools	Acceso
Pooneh Aref, Mehdi Ghoreyshi, Adam Jirasek and Matthew J. Satchell

Numerical Simulation of Heat Transfer and Chemistry in the Wake behind a Hypersonic Slender Body at Angle of Attack	Acceso
Matthew J. Satchell, Jeffrey M. Layng and Robert B. Greendyke

Prilling and Coating of Ammonium Dinitramide (ADN) Solid Green Propellant in Toluene Mixture Using Ultrasound Sonication	Acceso
Asad Rahman, Jitkai Chin and Kean How Cheah

Multi-UAV Doppler Information Fusion for Target Tracking Based on Distributed High Degrees Information Filters	Acceso
Hamza Benzerrouk, Alexander Nebylov and Meng Li

Field Trial Measurements to Validate a Stochastic Aircraft Boarding Model	Acceso
Michael Schultz

Experimental Study and Neural Network Modeling of Aerodynamic Characteristics of Canard Aircraft at High Angles of Attack	Acceso
Dmitry Ignatyev and Alexander Khrabrov

Design of a Facility for Studying Shock-Cell Noise on Single and Coaxial Jets	Acceso
Daniel Guariglia, Alejandro Rubio Carpio and Christophe Schram

Testing-Based Approach to Determining the Divergence Speed of Slung Loads	Acceso
Narayanan Komerath, Nandeesh Hiremath and Dhwanil Shukla

Experimental and Numerical Investigation of the Outer Ring Cooling Concept in a Hybrid and in an All-Steel Ball Bearing Used in Aero-Engines by the Introduction of a Helical Duct	Acceso
Michael Flouros, Peter Gloeckner, Markus Hirschmann, Matthias Martin, Francois Cottier and Dimitra Papailia

Predicting Non-Linear Flow Phenomena through Different Characteristics-Based Schemes	Acceso
Tom-Robin Teschner, L�szl� K�n�zsy and Karl W. Jenkins

Modeling and Dynamics of HTS Motors for Aircraft Electric Propulsion	Acceso
Ranjan Vepa

Rupture of a Cryogenic Composite Overwrapped Pressure Vessel Following a High-Speed Particle Impact	Acceso
William P. Schonberg

Thrust Augmentation by Airframe-Integrated Linear-Spike Nozzle Concept for High-Speed Aircraft	Acceso
Hidemi Takahashi, Toshihiko Munakata and Shigeru Sato

Robust Autoland Design by Multi-Model H8 Synthesis with a Focus on the Flare Phase	Acceso
Jean-Marc Biannic and Cl�ment Roos

Robust Control Design for Quad Tilt-Wing UAV	Acceso
Kai Masuda and Kenji Uchiyama

Discontinuous Galerkin Finite Element Investigation on the Fully-Compressible Navier?Stokes Equations for Microscale Shock-Channels	Acceso
Alberto Zingaro and L�szl� K�n�zsy

Fully-Deterministic Execution of IEC-61499 Models for Distributed Avionics Applications	Acceso
Carlos C. Insaurralde

Wake-Model Effects on Induced Drag Prediction of Staggered Boxwings	Acceso
Julian Schirra, William Bissonnette and G�tz Bramesfeld

Mathematical Modeling of Liquid-fed Pulsed Plasma Thruster	Acceso
Kaartikey Misra

Numerical Investigation on Windback Seals Used in Aero Engines	Acceso
Michael Flouros, Francois Cottier, Markus Hirschmann and Christina Salpingidou

Experimental Implementation of a Passive Millimeter-Wave Fast Sequential Lobing Radiometric Seeker Sensor	Acceso
Massimiliano Rossi, Riccardo Maria Liberati, Marco Frasca and Mauro Angelini

Formal Verification of Simulation Scenarios in Aviation Scenario Definition Language (ASDL)	Acceso
Bharvi Chhaya, Shafagh Jafer and Umut Durak

Pneumatically Powered Drilling of Carbon Fibre Composites Using Synthetic Biodegradable Lubricating Oil: An Experimental Study	Acceso
Corydon M. J. Morrell and Paul R. Hampson

Fast Aircraft Turnaround Enabled by Reliable Passenger Boarding	Acceso
Michael Schultz

Acknowledgement to Reviewers of Aerospace in 2017	Acceso
Aerospace Editorial Office

A Macroscopic Performance Analysis of NASA?s Northrop Grumman RQ-4A	Acceso
Enric Pastor, Marc P�rez-Batlle, Cristina Barrado, Pablo Royo and Ra�l Cuadrado

Preliminary Correlations for Remotely Piloted Aircraft Systems Sizing	Acceso
�lvaro G�mez-Rodr�guez, Alejandro Sanchez-Carmona, Luis Garc�a-Hern�ndez and Cristina Cuerno-Rejado

An Efficient Processing Architecture for Range Profiling Using Noise Radar Technology	Acceso
Davide Massaro, Riccardo Ardoino and Marco Grazzini

Application of an Efficient Gradient-Based Optimization Strategy for Aircraft Wing Structures	Acceso
Odeh Dababneh, Timoleon Kipouros and James F. Whidborne