PROCEEDINGS OF FIRST SHOCK TUBE SYMPOSIUM 26-27 FEBRUARY 1957
Abstract
Contents: Air Force Special Project's Interest in Shock tube Research; The Air Force Shock Tube as a Research Tool; Design and Performance of the General Electric Six-Inch Shock Tunnel Facility; The Development of a Shock Tube to Generate Variable Stepped Shock Fronts; Studies of Transient Air Forces on Two-Dimensional Airfoils; Studies of Grids in Shock Tubes; The Development of the Shock Tube Facility for Airfoil Studies; The Surface Film, Thermometer: A versatile Shock Tube Technique; Some Observations of Bifurcated Reflected Shock Waves; Numerical Solution for the Reflection of a Compression Wave from a Rigid Wall; The Use of the Shock Tube in Hypersonic Research; and Study of Re-entrant Corners.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1957
- Accession Number
- AD0467201
Entities
Organizations
- Air Force Special Weapons Center