Proceedings of the U.S. Air Force and The Federal Republic of Germany Data Exchange Agreement Meeting (9th), Viscous and Interacting Flow Field Effects Held at Silver Spring, Maryland on 9-10 May 1984,
Abstract
Contents: A Discrete Element Prediction Approach for Turbulent Flow Over Rough Surfaces; Mixing-Length Formulations for Turbulent Boundary Layers Over Arbitrarily Rough Surfaces; Shock/Boundary Layer Interaction Model for Three-Dimensional Transonic Flow Calculations; Boundary Layer Separation Due to Weak and Strong Viscous - Inviscid Interaction On An Inclined Body of Revolution; Experimental Study of Vortical Features in Three-Dimensional Separated Flow; Axisymmetric Bluff - Body Drag Reduction Through Geometrical Modifications; Experimental Investigations On Bodies With Noncircular Cross Sections In Compressible Flow (Pressure Distributions); Mach 3 Three-Dimensional Boundary Layer Turbulence Transport Properties On a Spherically Blunt Cone; An Experimental Investigation of The Stability of Laminar Boundary Layer On A Cone at M=8; Boundary Layer Transition On Blunt Slender Cones at MACH 10; Low Reynolds Number Hypersonic Testing in the NSWC Hypervelocity Wind Tunnel 9; Navier-Stokes Computations of Transonic Flow Over A Projectile With a Two-Equation Model of Turbulence; P.N.S. Computations for Non-Circular and Finned Body Configurations At Supersonic Velocities; Effects of Propulsive Jet On The Flow Field in the Tail Region of a Missile in a Supersonic Stream; and Navier-Stokes Calculations of Base Region Flow Fields for Bodies of Revolution.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1984
- Accession Number
- ADA153020
Entities
People
- A. W. Fiore
Organizations
- Wright Laboratory