ISSN: 0021-8669

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Journal of Aircraft Q1 Unclaimed

American Institute of Aeronautics and Astronautics Inc. (AIAA) United States

Unfortunately this journal has not been claimed yet. For this reason, some information may be unavailable.

Journal of Aircraft is a journal indexed in SJR in Aerospace Engineering with an H index of 107. It has an SJR impact factor of 0,911 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 0,911.

Type: Journal

Type of Copyright:

Languages: English

Open Access Policy:

Type of publications:

Publication frecuency: -

Categories: Aerospace Engineering (Q1)

Price

- €

Inmediate OA

NPD

Embargoed OA

- €

Non OA

Metrics

0,911

SJR Impact factor

107

H Index

117

Total Docs (Last Year)

328

Total Docs (3 years)

4911

Total Refs

759

Total Cites (3 years)

309

Citable Docs (3 years)

1.89

Cites/Doc (2 years)

41.97

Ref/Doc

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IEEE Transactions on Vehicular Technology Q1
Progress in Aerospace Sciences Q1
Mechanical Systems and Signal Processing Q1
Transportation Research Part A: Policy and Practice Q1
International Journal of Mechanical Sciences Q1

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Aims and Scope

Best articles by citations

Design-Oriented High-Lift Methodology for General Aviation and Civil Transport Aircraft

Flow-Separation Lines on Axisymmetric Bodies with Tapered Tails

Enriched Basis Functions for Handling Wake-Body Intersections in Dirichlet Panel Methods

Nature of Wakelike and Jetlike Axial Tip Vortex Flows

Experimental Study on Aircraft Landing Gear Noise

Two-dimensional air-cushion vehicle critical forward speeds.

Prediction of Flow Dynamics over Cavities by Detached Eddy Simulation

Flight Control Using Wing-Tip Plasma Actuation

Rapid prediction of high-alpha unsteady aerodynamics of slender-wingaircraft

Declining Angle Effects of the Trailing Edge of a Microramp Vortex Generator

Poststall Prediction of Multiple-Lifting-Surface Configurations Using a Decambering Approach

Development of a Four-Rotor Cyclocopter

SHOW MORE ARTICLES

Development of Variable Camber Morphing Airfoil Using Corrugated Structure

Air-Vessel Corrosion Damage Distribution and Reliability Modeling

Minimizing Induced Drag with Spanwise Blowing Variation on Circulation-Controlled Wing

Nonlinear aerodynamics of a two-dimensional membrane airfoil with separation

Drag and wake modification of axisymmetric bluff bodies using Coanda blowing

Investigation on Transonic Correction Methods for Unsteady Aerodynamics and Aeroelastic Analyses

Drag Polar Invariance with Flexibility

Flight Testing the Parachute System for the Space Station Crew Return Vehicle

Transport Aircraft Wake Influenced by a Large Winglet and Winglet Flaps

Design of Low Reynolds Number Airfoils with Trips

Survey and comparison of engineering beam theories for helicopter rotor blades

Flight through thunderstorm outflows