Accession Number:

AD0909223

Title:

Proceedings of the Boundary Layer Transition Workshop Held 3-5 November 1971. Volume 3

Descriptive Note:

Technical operating rept.

Corporate Author:

AEROSPACE CORP SAN BERNARDINO CA SAN BERNARDINO OPERATIONS

Personal Author(s):

Report Date:

1971-12-20

Pagination or Media Count:

312.0

Abstract:

Contents Effects of Mass Addition Distribution and Roughness on Boundary Layer Transition at Mach 12 Effects of Nose Bluntness and Free-Stream Unit Reynolds Number on Slender Cone Transition at Hypersonic Speeds Free Flight Determination of Boundary Layer Transition on Small Scale Cones in the Presence of Surface Ablation Effects of Wall Cooling and Angle of Attack on Boundary-Layer Transition on Sharp Cones at Free Stream Mach no. 7.4 Some Special Features of Boundary Layer Transition on Aeroballistic Range Models Hypersonic Simulation for Lifting Body Transition Studies Effect of Transition on Three-Dimensional Shock Wave-Boundary Layer Interaction Hypersonic Shock Tunnel Transition Studies Open Questions - Transition to Turbulence at High Speeds and Lessons from Transition of Shock-Tube Boundary Layers.

Subject Categories:

  • Aerodynamics
  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Guided Missile Reentry Vehicles
  • Spacecraft Trajectories and Reentry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE