AIAA Scitech 2019 Forum
Latest Publications

TOTAL DOCUMENTS

2599

(FIVE YEARS 2599)

H-INDEX

(FIVE YEARS 11)

Published By American Institute Of Aeronautics And Astronautics

9781624105784

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Correction: Experimental Investigation of the NASA Common Research Model with a Natural Laminar Flow Wing in the NASA Langley National Transonic Facility

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-2189.c1 ◽

2019 ◽

Author(s):

Melissa B. Rivers ◽

Michelle N. Lynde ◽

Richard L. Campbell ◽

Sally A. Viken ◽

David T. Chan ◽

...

Keyword(s):

Experimental Investigation ◽

Laminar Flow ◽

Research Model ◽

Natural Laminar Flow

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Correction: Pilot Workload Estimation: Synthesis of Spectral Requirements Analysis and Weber’s Law

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1228.c1 ◽

2019 ◽

Author(s):

Edward N. Bachelder ◽

Martine Godfroy-Cooper

Keyword(s):

Requirements Analysis ◽

Weber’S Law ◽

Weber's Law

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Correction: Nonlinear Aeroelasticity: a CFD-based Adaptive Methodology for Flutter Prediction

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1866.c1 ◽

2019 ◽

Author(s):

Rocco Bombardieri ◽

Rauno Cavallaro ◽

Jorge Luis Sáez de Teresa ◽

Moti Karpel

Keyword(s):

Nonlinear Aeroelasticity

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Correction: Multidisciplinary Optimization and Performance Analysis Tool for Ballistic Missiles

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1972.c1 ◽

2019 ◽

Author(s):

Misra A. Adsiz ◽

Ali Turker Kutay

Keyword(s):

Performance Analysis ◽

Multidisciplinary Optimization ◽

Analysis Tool ◽

Ballistic Missiles ◽

And Performance ◽

Optimization And Performance

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Correction: Wall bounded turbulent flows up to high Reynolds numbers: LES resolution assessment

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1887.c1 ◽

2019 ◽

Author(s):

Ghazaleh Ahmadi ◽

Hassan Kassem ◽

Bernhard Stoevesandt ◽

Joachim Peinke ◽

Stefan Heinz

Keyword(s):

Turbulent Flows ◽

Reynolds Numbers ◽

High Reynolds Numbers ◽

High Reynolds

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Withdrawal: Numerical Simulation of Variable-Geometry TBCC Inlet with Smoothly Slid Mechanism

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-0945.c1 ◽

2019 ◽

Author(s):

Ting Yue ◽

Guoping Huang ◽

Chen Xia

Keyword(s):

Numerical Simulation ◽

Variable Geometry

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Correction: Analysis of Limit-Cycle Oscillation in Control Systems with Piecewise Nonlinearities

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-2182.c1 ◽

2019 ◽

Author(s):

Yong Eun Yoon ◽

Eric N. Johnson

Keyword(s):

Control Systems ◽

Limit Cycle ◽

Limit Cycle Oscillation ◽

Cycle Oscillation

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Boundary layer transition detection on wind tunnel models in PETW during continuous pitch traverse

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1180 ◽

2019 ◽

Cited By ~ 2

Author(s):

Christian Klein

Keyword(s):

Boundary Layer ◽

Wind Tunnel ◽

Boundary Layer Transition ◽

Layer Transition

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Withdrawal: Computations of Aerodynamic Behaviour of Small Horizontal Axis Wind Turbine with NACA4418 airfoil

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-1277.c1 ◽

2019 ◽

Author(s):

Essam E. Khalil ◽

Gamal E. ElHarriri ◽

Eslam E. AbdelGhany ◽

Moemen E. Farghaly

Keyword(s):

Wind Turbine ◽

Horizontal Axis ◽

Horizontal Axis Wind Turbine

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Correction: Multidisciplinary System Design Optimization Approach for Lunar Surface Access from Cislunar Orbit

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-0702.c1 ◽

2019 ◽

Author(s):

Satoshi Ueda ◽

Toshinori Ikenaga ◽

Ryo Ujiie

Keyword(s):

Design Optimization ◽

System Design ◽

Lunar Surface ◽

Optimization Approach ◽

System Design Optimization ◽

Multidisciplinary System

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AIAA Scitech 2019 ForumLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Correction: Experimental Investigation of the NASA Common Research Model with a Natural Laminar Flow Wing in the NASA Langley National Transonic Facility

Correction: Pilot Workload Estimation: Synthesis of Spectral Requirements Analysis and Weber’s Law

Correction: Nonlinear Aeroelasticity: a CFD-based Adaptive Methodology for Flutter Prediction

Correction: Multidisciplinary Optimization and Performance Analysis Tool for Ballistic Missiles

Correction: Wall bounded turbulent flows up to high Reynolds numbers: LES resolution assessment

Withdrawal: Numerical Simulation of Variable-Geometry TBCC Inlet with Smoothly Slid Mechanism

Correction: Analysis of Limit-Cycle Oscillation in Control Systems with Piecewise Nonlinearities

Boundary layer transition detection on wind tunnel models in PETW during continuous pitch traverse

Withdrawal: Computations of Aerodynamic Behaviour of Small Horizontal Axis Wind Turbine with NACA4418 airfoil

Correction: Multidisciplinary System Design Optimization Approach for Lunar Surface Access from Cislunar Orbit

AIAA Scitech 2019 Forum
Latest Publications