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期刊名：Aiaa journal

缩写：AIAA J

ISSN：0001-1452

e-ISSN：1533-385X

IF/分区：3.2/Q1

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共收录本刊相关文章索引3962条
Clinical Trial Case Reports Meta-Analysis RCT Review Systematic Review
Classical Article Case Reports Clinical Study Clinical Trial Clinical Trial Protocol Comment Comparative Study Editorial Guideline Letter Meta-Analysis Multicenter Study Observational Study Randomized Controlled Trial Review Systematic Review
Investigation of natural frequencies and mode shapes of buckled beams [0.03%]
AIAA Journal. 1995;33(6):1121-1126. DOI:10.2514/3.12669 1995
Numerical Study of the Control of Tollmien–Schlichting Waves Using Plasma Actuators [0.03%]
Kotsonis, Marios; Giepman, Rogier; Hulshoff et al. Kotsonis et al.
AIAA Journal. 2013;51(10):2353-2364. DOI:10.2514/1.J051766 2013
Nitric-Oxide Planar Laser-Induced Fluorescence Measurements in the Hypersonic Materials Environmental Test System [0.03%]
Inman, Jennifer A.; Bathel, Brett F.; Johansen et al. Inman et al.
AIAA Journal. 2013;51(10):2365-2379. DOI:10.2514/1.J052246 2013
Optimization of coupled systems - A critical overview of approaches [0.03%]
Balling, R. J.; Sobieszczanski-Sobieski, J. Balling
AIAA Journal. 1996;34(1):6-17. DOI:10.2514/3.13015 1996
General thermal constriction parameter for annular contacts on circular flux tubes [0.03%]
AIAA Journal. 1976;14(6):822-824. DOI:10.2514/3.7158 1976
Spatial transformation of the discrete sound field from a propeller [0.03%]
AIAA Journal. 1996;34(6):1097-1102. DOI:10.2514/3.13198 1996
Inverse aeroacoustic problem for a streamlined body. I - Basic formulation [0.03%]
Grace, Sheryl P.; Atassi, Hafiz M.; Blake et al. Grace et al.
AIAA Journal. 1996;34(11):2233-2240. DOI:10.2514/3.13385 1996
Inverse aeroacoustic problem for a streamlined body. II - Accuracy of solutions [0.03%]
Grace, Sheryl P.; Atassi, Hafiz M.; Blake et al. Grace et al.
AIAA Journal. 1996;34(11):2241-2246. DOI:10.2514/3.13386 1996
Inverse Aeroacoustic Problem for a Rectangular Wing [0.03%]
Wood, Trevor H.; Grace, Sheryl M. Wood
AIAA Journal. 2000;38(2):203-210. DOI:10.2514/2.963 2000
Vortex/separated boundary-layer interactions at transonic Mach numbers [0.03%]
MEHTA, RABINDRA D. MEHTA
AIAA Journal. 1988;26(1):15-26. DOI:10.2514/3.9845 1988