Journal of the American Helicopter Society
Journal of the American Helicopter Society is a journal indexed in SJR in Materials Science (miscellaneous) and Mechanical Engineering with an H index of 62. It has an SJR impact factor of 0,729 and it has a best quartile of Q1. It is published in English. It has an SJR impact factor of 0,729.
Metrics
Scimago and CountryOfPapers database fields
SJR Impact
0,729
H-index
62
Docs (year)
43
Docs 3y
135
Total refs
1462
Cites 3y
326
Citable 3y
135
Cites/Doc 2y
2.49
Ref/Doc
34.0
Immediate OA
—
Embargoed OA
NPD
Non OA / Submission
—
Name good journals. Call out predatory ones.
Share what peer review, fees, and timelines were really like. Praise fair editors. Flag APC traps, fake metrics, or spam solicitations — with facts from your submission.
Researcher reviews
Best articles by citations
An Engineering Modification of the Blade Element Momentum Equation for Vertical Descent: An Autorotation Case Study
View moreXVhyphen;15 Aeroacoustic Testing at NASA Ames
View moreComputation of Helicopter Fuselage Aerodynamics Using Navier-Stokes CFD Methods
View moreCompressive Failure Mechanisms in Composite Sandwich Structures
View moreCompressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap
View moreComposite Skid Landing Gear Performance and Laminate Tailoring for Reduced Load Factor under Limit Loads
View moreComposite Skid Landing Gear Design Feasibility
View moreBuckling Interaction in Regular Arrays of Rigidly Supported Composite Laminated Plates with Orthogrid, Isogrid, and Anisogrid Planform
View moreBroadband Helicopter Noise Generated by Blade Wake Interactions
View moreBook Review: Rotary Wing Structural Dynamics and Aeroelasticity, 2nd Edition by Richard L. Bielawa
View moreBlade-Vortex Interaction Airloads Prediction Using Coupled Computational Fluid and Structural Dynamics
View moreAnalysis and Tests of Reinforced Carbon-Epoxy/Foam-Core Sandwich Panels with Cutouts
View moreAn Implicit Floquet Analysis for Rotorcraft Stability Evaluation
View moreA Comparison of Measured and Predicted XV-15 Tiltrotor Surface Acoustic Pressures
View moreAn Empirical Correction for Improving Off-Axes Response in Flight Mechanics Helicopter Models
View moreAn Effective Crashworthiness Design Optimization Methodology to Improve Helicopter Landing Gear Energy Absorption
View moreAeroelastic Analysis of Rotors with Trailing Edge Flaps Using Comprehensive Codes
View moreAcoustic Wind Tunnel Tests on Helicopter Tail Rotor Noise (HeliNOVI)
View moreA Variational Method for Computing the Optimal Aerodynamic Performance of Conventional and Compound Helicopters
View moreA Prospective: The Importance of Propulsion Technology to the Development of Helicopter Systems with a Vision for the Future The 27th Alexander A. Nikolsky Lecture
View moreA Parametric Design Study for Actively Controlled Trailing Edge Flaps
View moreA Numerical Study of Sand Separation Applicable to Engine Inlet Particle Separator Systems
View moreA Method to Predict Acoustic Scattering of Rotorcraft Noise
View moreA Critical Evaluation of Various Approaches for the Numerical Detection of Helicopter Blade-Vortex Interactions
View more