LEADING EDGES DEVELOPMENT - DYNA SOAR. VOLUME 3 THERMAL GRADIENT AND LOADS TEST DATA
Abstract
Contents: tabulated temperature data, tabulated pressure load vs. deflection data, tabulated pressure load vs. maximum shear stress and principal stress data, rapid load vs. time curves, tabulated rapid load vs. deflection data, tabulated slow load vs. deflection data, and tolerances for thermocouples.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 25, 1963
- Accession Number
- AD0421685
Entities
People
- D. A. Bowers
- Paul G. Esch
Organizations
- Boeing