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Journal of Aircraft is a peer-reviewed journal published by AIAA, covering Computational Fluid Dynamics and Aerodynamics, Fluid Dynamics and Turbulent Flows, Aerospace and Aviation Technology. Over its lifetime it has published 11,396 papers, which have received 220,533 citations.
| Publisher | AIAA |
|---|---|
| Reference style | Numbered (AIAA) Numbered — [1], [2] in the text [1] Smith, A., Jones, B., and Lee, C., "A Representative Article Title," Journal of Aircraft, Vol. 12, No. 3, 2023, pp. 45–58.
Formats any DOI in Journal of Aircraft style. No sign-up. |
| Publishes research in | Computational Fluid Dynamics and Aerodynamics Fluid Dynamics and Turbulent Flows Aerospace and Aviation Technology Aerodynamics and Acoustics in Jet Flows Advanced Aircraft Design and Technologies |
| ISSN | 0021-8669 |
| Citation impact (2-yr) | 1.55 |
| h-index | 139 |
| i10-index | 5,363 |
| Top institutions publishing here | Langley Research Center |
| Journal website | arc.aiaa.org |
| You get | A submission-ready PDF and the editable LaTeX source — ready to submit. |
Citations each year’s papers have accumulated so far — the most recent years are still building up.
A study was conducted to assess the feasibility of performing computerized wing design by numerical optimization. The design program combined a full potential, inviscid aerodynamics code with a conjugate gradient optimization algorithm. Three design problems were selected to demonstrate the design technique. The first involved modifying the upper surface of the inboard 50% of a…
andsimplemathematicalfunctionshavingeasilyobservedphysicalfeatures.Thefundamentalparametricgeometry representation method is shown to describe an essentially limitless design space composed entirely of analytically smooth geometries. The class function/shape function methodology is then extended to more general threedimensional applications such as wing, body, ducts, and nacelles. It is shown that a general three-dimensional geometry can be represented by a distribution of fundamental shapes,…
TheBoeingBlended-Wing–Body (BWB)airplane concept represents a potentialbreakthrough in subsonic trans-port ef ciency. Work began on this concept via a study to demonstrate feasibility and begin development of this new class of airplane. In this initial study, 800-passengerBWB and conventionalcon guration airplaneswere sized and compared for a 7000-n mile design range. Both airplanes were based on engine…
A surface spline is a mathematical tool for interpolating a function of two variables. It is based upon the small deflection equation of an infinite plate. The surface spline depends upon the solution of a system of linear equations, and thus, will ordinarily require the use of a digital computer. The closed form solution involves…
