NATO RTO AVT Task Group-080 "Vortex Breakdown over Slender Wings": Objectives and Overview

[1]  Xing-Zhong Huang,et al.  Nonlinear Indicial Response and Internal State-Space Representation and Its Applications on Delta Wing Aerodynamics , 2003 .

[2]  T. Ohlemiller,et al.  Radiative Ignition of Double Base Propellants: II. Pre-ignition Events and Source Effects , 1973 .

[3]  Anthony Mitchell,et al.  Experimental Data Base Selected for RTO/AVT Numerical and Analytical Validation and Verification: ONERA 70-deg Delta Wing , 2003 .

[4]  N. Verhaagen,et al.  Effects of Sideslip on the Characteristics of a 65-deg Delta Wing , 2003 .

[5]  Scott A. Morton,et al.  High Reynolds Number DES Simulations of Vortex Breakdown over a 70 Degree Delta Wing , 2003 .

[6]  A Simple Engineering Model for Vortex Breakdown , 2003 .

[7]  Xing-Zhong Huang Comprehensive Experimental Studies on Vortex Dynamics over Military Wing Configurations in IAR , 2003 .

[8]  R. K. Nangia Applying Vortex Breakdown Empiricisms to Predict Aerodynamic Characteristics in Symmetric and Asymmetric Situations , 2003 .

[9]  Marcel Escudier,et al.  Vortex breakdown: Observations and explanations , 1988 .

[10]  Ismet Gursul,et al.  Review of Unsteady Vortex Flows Over Delta Wings , 2003 .

[11]  Robert C. Nelson,et al.  The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers , 2003 .

[12]  Miguel R. Visbal,et al.  On the Structure of the Shear Layer Emanating from a Swept Leading Edge at Angle of Attack , 2003 .

[13]  Stefan Görtz,et al.  Time-accurate Euler Simulations of a Full-Span Delta Wing at High Incidence , 2003 .

[14]  Bambang Soewarmoto,et al.  Numerical Investigation of Vortical Flows Using RANS Equations , 2003 .

[15]  J. Délery Aspects of vortex breakdown , 1994 .

[16]  Mark Allan,et al.  A CFD investigation of wind tunnel interference on delta wing aerodynamics , 2003 .

[17]  J. A. Bagley Some aerodynamic principles for the design of swept wings , 1962 .

[18]  S. Görtz Detached-Eddy Simulations of a Full-Span Delta Wing at High Incidence , 2003 .