Add to ORKGThe aerodynamic effect of heavy rain on airplane performance is presented in the form of view-graphs. The following subject areas are covered: review of heavy rain airfoil tests; development of heavy rain aerodynamic model for a twin-jet transport; performance analysis with heavy rain effects; numeric simulation of wet microburst encounter; and summary of results and future needs
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
The effects were studied of visual display dynamics on pilot tracking performance in a simulator. Th...
A weight-measuring rain gauge was developed to collect rain data and configured to operate at a high...
The shuttle descends along a rather shallow path, thus providing some information on the horizontal ...
The current program is aimed at providing a physical picture of the flow physics and quantitative tu...
High bypass geared turbofan engines with nacelles forming the propulsion system for short-haul passe...
Space transportation avionics technology operational efficiency issues are presented in viewgraph fo...
Development of a steady flow solver for use with LINFLO was the objective of this report. The solver...
Two X-29A aircraft were flown at the NASA Dryden Flight Research Center over a period of eight years...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
One of the powered lift systems currently being considered for use on STOL vehicles obtains addition...
The objective of this research is to simulate steady and unsteady viscous flows, including rotor/sta...
General overview of NASA/Langley Research Center wind shear flight project is presented in the form ...
A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered inc...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
The effects were studied of visual display dynamics on pilot tracking performance in a simulator. Th...
A weight-measuring rain gauge was developed to collect rain data and configured to operate at a high...
The shuttle descends along a rather shallow path, thus providing some information on the horizontal ...
The current program is aimed at providing a physical picture of the flow physics and quantitative tu...
High bypass geared turbofan engines with nacelles forming the propulsion system for short-haul passe...
Space transportation avionics technology operational efficiency issues are presented in viewgraph fo...
Development of a steady flow solver for use with LINFLO was the objective of this report. The solver...
Two X-29A aircraft were flown at the NASA Dryden Flight Research Center over a period of eight years...
To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for ...
One of the powered lift systems currently being considered for use on STOL vehicles obtains addition...
The objective of this research is to simulate steady and unsteady viscous flows, including rotor/sta...
General overview of NASA/Langley Research Center wind shear flight project is presented in the form ...
A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered inc...
Pressures were simultaneously measured in the variable-density tunnel at 54 orifices distributed ove...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
The effects were studied of visual display dynamics on pilot tracking performance in a simulator. Th...