Accession Number : ADA111783

Title :   Proceedings of the Navy Symposium on Aeroballistics (12th) Held at the David Taylor Naval Ship Research and Development Center, Bethesda, Maryland on 12-13-14 May 1981. Volume II.


PDF Url : ADA111783

Report Date : 14 May 1981

Pagination or Media Count : 366

Abstract : Contents: Current Status of Inlet Flow Prediction Methods; Rotational Flow in a Curved-Wall Diffuser Designed by Using the Inverse Method of Solution of Potential Flow Theory; Aerodynamic Characteristics of a Series of Airbreathing Missile Configurations; Parabolized Navier-Stokes Predictions for Three-Dimensional Viscous Supersonic Flows; Results of a Government and Industry Survey of the Heating Methods Used to Determine Missile Structural Temperatures; Supersonic Combustor Insulation Ablation Analysis and Tests; Computation of Three-Dimensional Viscous Flow over Blunt Lifting Bodies at High Angle of Attack; Computation of Hypersonic Laminar Viscous Flow over a Body with Mass Transfer and/or Spin at Angle of Attack; Three-Dimensional Viscous Shock-Layer Analysis of Laminar or Turbulent Flows in Chemical Equilibrium; Further Development of the Streamline Method for Determination of Three-Dimensional Flow Separation; Comparison of Numerical Results and Measured Data for Smooth and Indented Nosetips; Structural and Electrical Performance Considerations in the Design of Multiband Radomes; and Structural Considerations for the Recovery of Air-to-Air Missiles.

Descriptors :   *Aeroballistics, *Symposia, Jet engine inlets, Flow fields, Diffusers, Air breathing engines, Navier stokes equations, Supersonic flow, Hypersonic flow, Combustors, Shock, Flow separation, Nose tips, Radomes, Guided missiles

Subject Categories : Guided Missiles
      Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE