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Directory Listing of /edt/manual/Magazine/A/AIAA Journal of Aircraft US/1990/6/

Folder.. - Mar 05 2025 11:57:13 PM
Acoustics of ultralight airplanes c20030709 [7].pdfAcoustics of ultralight airplanes c20030709 [7].pdf 1296KB Mar 29 2010 10:58:06 AM
Analyses of Arrow Air DC-8-63 accident of December 12, 1985 - Gander, Newfoundland c20030709 [8].pdfAnalyses of Arrow Air DC-8-63 accident of December 12, 1985 - Gander, Newfoundland c20030709 [8].pdf 983KB Mar 29 2010 10:58:06 AM
ATTENTION JOURNAL AUTHORS c20030709 [1].pdfATTENTION JOURNAL AUTHORS c20030709 [1].pdf 133KB Mar 29 2010 10:58:06 AM
Comparison of high-angle-of-attack slender-body theory and exact solutions for potential flow over an ellipsoid c20030709 [3].pdfComparison of high-angle-of-attack slender-body theory and exact solutions for potential flow over an ellipsoid c20030709 [3].pdf 358KB Mar 29 2010 10:58:06 AM
Determination of aerodynamic sensitivity coefficients based on the transonic small perturbation formulation c20030709 [9].pdfDetermination of aerodynamic sensitivity coefficients based on the transonic small perturbation formulation c20030709 [9].pdf 987KB Mar 29 2010 10:58:06 AM
Drag measurements on a modified prolate spheroid using a magnetic suspension and balance system c20030709 [6].pdfDrag measurements on a modified prolate spheroid using a magnetic suspension and balance system c20030709 [6].pdf 1210KB Mar 29 2010 10:58:06 AM
Drag reduction by controlling flow separation using stepped afterbodies c20030709 [3].pdfDrag reduction by controlling flow separation using stepped afterbodies c20030709 [3].pdf 324KB Mar 29 2010 10:58:06 AM
Effect of detailed surface geometry on riblet drag reduction performance c20030709 [2].pdfEffect of detailed surface geometry on riblet drag reduction performance c20030709 [2].pdf 677KB Mar 29 2010 10:58:06 AM
Flow structure generated by oscillating delta-wing segments c20030709 [3].pdfFlow structure generated by oscillating delta-wing segments c20030709 [3].pdf 487KB Mar 29 2010 10:58:06 AM
Flow visualization studies of the Mach number effects on dynamic stall of an oscillating airfoil c20030709 [7].pdfFlow visualization studies of the Mach number effects on dynamic stall of an oscillating airfoil c20030709 [7].pdf 1196KB Mar 29 2010 10:58:06 AM
Hypervelocity, minimum-radii, coordinated turns c20030709 [4].pdfHypervelocity, minimum-radii, coordinated turns c20030709 [4].pdf 431KB Mar 29 2010 10:58:06 AM
Improved, robust, axial line singularity method for bodies of revolution c20030709 [7].pdfImproved, robust, axial line singularity method for bodies of revolution c20030709 [7].pdf 800KB Mar 29 2010 10:58:06 AM
Investigation of the near wake of a propfan c20030709 [7].pdfInvestigation of the near wake of a propfan c20030709 [7].pdf 789KB Mar 29 2010 10:58:06 AM
Sidewall boundary-layer removal and wall adaptation studies c20030709 [6].pdfSidewall boundary-layer removal and wall adaptation studies c20030709 [6].pdf 860KB Mar 29 2010 10:58:06 AM
Static aeroelastic tailoring for oblique wing lateral trim c20030709 [6].pdfStatic aeroelastic tailoring for oblique wing lateral trim c20030709 [6].pdf 909KB Mar 29 2010 10:58:06 AM
Strake camber and thickness design procedure for low alpha supersonic flow c20030709 [7].pdfStrake camber and thickness design procedure for low alpha supersonic flow c20030709 [7].pdf 1443KB Mar 29 2010 10:58:06 AM
Various sources of wing rock c20030709 [7].pdfVarious sources of wing rock c20030709 [7].pdf 821KB Mar 29 2010 10:58:06 AM