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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1989/1/

Folder.. - Mar 05 2025 11:56:11 PM
1989 - A _Building Frame_ c20030709 [1].pdf1989 - A _Building Frame_ c20030709 [1].pdf 151KB Mar 29 2010 10:54:38 AM
AIAA Manuscript Review Process c20030709 [1].pdfAIAA Manuscript Review Process c20030709 [1].pdf 149KB Mar 29 2010 10:54:38 AM
Analytic prediction of the maximum amplitude of slender wing rock c20030709 [5].pdfAnalytic prediction of the maximum amplitude of slender wing rock c20030709 [5].pdf 717KB Mar 29 2010 10:54:38 AM
Application of a full potential method to supersonic aircraft designand analysis c20030709 [7].pdfApplication of a full potential method to supersonic aircraft designand analysis c20030709 [7].pdf 794KB Mar 29 2010 10:54:38 AM
Euler procedure for three-dimensional transonic wall interference c20030709 [8].pdfEuler procedure for three-dimensional transonic wall interference c20030709 [8].pdf 1082KB Mar 29 2010 10:54:38 AM
Further generalization of an equivalent plate representation for aircraft structural analysis c20030709 [8].pdfFurther generalization of an equivalent plate representation for aircraft structural analysis c20030709 [8].pdf 1084KB Mar 29 2010 10:54:38 AM
Improvements to an Euler aerodynamic method for transonic flow analysis c20030709 [8].pdfImprovements to an Euler aerodynamic method for transonic flow analysis c20030709 [8].pdf 971KB Mar 29 2010 10:54:38 AM
Integrated aeroservoelastic analysis capability with X-29A comparisons c20030709 [7].pdfIntegrated aeroservoelastic analysis capability with X-29A comparisons c20030709 [7].pdf 700KB Mar 29 2010 10:54:38 AM
Measurements of propeller noise in a light turboprop airplane c20030709 [8].pdfMeasurements of propeller noise in a light turboprop airplane c20030709 [8].pdf 1100KB Mar 29 2010 10:54:38 AM
Numerical study of a research circulation control airfoil using Navier-Stokes methods c20030709 [6].pdfNumerical study of a research circulation control airfoil using Navier-Stokes methods c20030709 [6].pdf 869KB Mar 29 2010 10:54:38 AM
Reviewers for the Journal of Aircraft - 1988 _ c20030709 [1].pdfReviewers for the Journal of Aircraft - 1988 _ c20030709 [1].pdf 114KB Mar 29 2010 10:54:38 AM
Self-preservation of turbulent wakes c20030709 [4].pdfSelf-preservation of turbulent wakes c20030709 [4].pdf 493KB Mar 29 2010 10:54:38 AM
Separated flows developing under increasingly adverse pressure gradients c20030709 [3].pdfSeparated flows developing under increasingly adverse pressure gradients c20030709 [3].pdf 396KB Mar 29 2010 10:54:38 AM
Similarity for high-angle-of-attack subsonic transonic slender-body aerodynamics c20030709 [11].pdfSimilarity for high-angle-of-attack subsonic transonic slender-body aerodynamics c20030709 [11].pdf 1059KB Mar 29 2010 10:54:38 AM
Supersonic flutter of aeroelastically tailored oblique wings c20030709 [9].pdfSupersonic flutter of aeroelastically tailored oblique wings c20030709 [9].pdf 1151KB Mar 29 2010 10:54:38 AM
The 1989 Team c20030709 [2].pdfThe 1989 Team c20030709 [2].pdf 695KB Mar 29 2010 10:54:38 AM
Unsteady transonic flow calculations for realistic aircraft configurations c20030709 [8].pdfUnsteady transonic flow calculations for realistic aircraft configurations c20030709 [8].pdf 1111KB Mar 29 2010 10:54:38 AM