Call Number (LC) | Title | Results |
---|---|---|
NAS 1.15:86759 | On blockage corrections for two-dimensional wind tunnel tests using the wall-pressure signature method | 1 |
NAS 1.15:86760 |
A review of shock waves around aeroassisted orbital transfer vehicles A review of shock waves around aeroassisted orbital transfer vehicles / |
2 |
NAS 1.15:86761 | Viscous flows in rotating pipes with internal cavities and related vortex breakdowns | 1 |
NAS 1.15:86762 | Flight testing the fixed-wing configuration of the rotor systems research aircraft (RSRA) | 1 |
NAS 1.15:86763 | Prediction of the flow-field interference induced by the long range laser velocimeter in the Ames 40- by 80- foot and the 80- by 120-foot wind tunnels | 1 |
NAS 1.15:86764 | ||
NAS 1.15:86766 | ||
NAS 1.15:86768 | A three-dimensional turbulent boundary layer undergoing transverse strain and streamwise pressure gradient | 1 |
NAS 1.15:86770 | Catalytic surface effects on contaminated space shuttle tiles in a dissociated nitrogen stream | 1 |
NAS 1.15:86771 | Transonic rotor tip design using numerical optimization | 1 |
NAS 1.15:86772 | Development of a new laser Doppler velocimeter for the Ames High Reynolds Channel No. 2 | 1 |
NAS 1.15:86773 | Simulation of complex three-dimensional flows | 1 |
NAS 1.15:86774 | ||
NAS 1.15:86775 |
Generalized formulation of a class of explicit and implicit TVD schemes / Generalized formulation of a class of explicit and implicit TVD schemes |
2 |
NAS 1.15:86776 | Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / | 2 |
NAS 1.15:86777 | Some recent advances in computational aerodynamics for helicopter applications | 1 |
NAS 1.15:86778 | Relative advantages of thin-layer Navier-Stokes and interactive boundary-layer procedures | 1 |
NAS 1.15:86779 | Simulation evaluation of display-FLAIR concepts for low altitude terrain-following helicopter operations | 1 |
NAS 1.15:86780 | Computation of three-dimensional shock wave and boundary-layer interactions | 1 |
NAS 1.15:86781 | Shock fitting applied to the prediction of high-speed rotor noise | 1 |