Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7 results returnedSearch results
- Laminar friction and heat transfer at Mach numbers from 1 to 10
- Effect of a finite trailing-edge thickness on the drag of rectangular and delta wings at supersonic speeds
- Comparison of supersonic minimum-drag airfoils determined by linear and nonlinear theory
- Effect of thermal properties on laminar-boundary-layer characteristics
- On slender-body theory at transonic speeds
- Some considerations of the influence of body cross-sectional shape on the lifting efficiency of wing-body combinations at supersonic speeds
- General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces