Add to ORKGExperiments with planing surfaces are fundamental, hydrodynamic researches for the purpose of obtaining the most favorable forms for planing boats, flying boats, and seaplane floats, with respect to water resistance and seaworthiness
In this paper the support system interference on the zero lift drag of an axisymmetric and an aircra...
A Boltz body of revolution (fineness ratio 7.5:1) was tested in the Southampton University Magnetic ...
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
The problems of large-angle attitude maneuvers of a spacecraft have gained much consideration in rec...
Experimental measurements are reported, on the velocity fields and turbulence parameters on a water ...
For the purpose of solving all the problems involved, an investigation was made with flat, rectangul...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
This report is directed to the problem of developing an adequate but not overly complex linear fligh...
In the present paper we shall consider a figure of revolution, so that the formulas applicable to th...
This report describes the results of a small study program in support of the design studies for NASA...
The take-off capacity of a flying boat depends upon the design of the hull bottom ahead as well as a...
Closed-form equations for the lift, drag, and pitching moment coefficients of two dimensional airfoi...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
The Discovery vehicle was found to have longitudinal and lateral aerodynamic characteristics similar...
Structural dynamic environmental test levels were developed for the thematic mapper instrument, comp...
In this paper the support system interference on the zero lift drag of an axisymmetric and an aircra...
A Boltz body of revolution (fineness ratio 7.5:1) was tested in the Southampton University Magnetic ...
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...
The problems of large-angle attitude maneuvers of a spacecraft have gained much consideration in rec...
Experimental measurements are reported, on the velocity fields and turbulence parameters on a water ...
For the purpose of solving all the problems involved, an investigation was made with flat, rectangul...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
This report is directed to the problem of developing an adequate but not overly complex linear fligh...
In the present paper we shall consider a figure of revolution, so that the formulas applicable to th...
This report describes the results of a small study program in support of the design studies for NASA...
The take-off capacity of a flying boat depends upon the design of the hull bottom ahead as well as a...
Closed-form equations for the lift, drag, and pitching moment coefficients of two dimensional airfoi...
An advanced-design 25-foot-diameter flightworthy proprotor was tested in the NASA-Ames Large-Scale W...
The Discovery vehicle was found to have longitudinal and lateral aerodynamic characteristics similar...
Structural dynamic environmental test levels were developed for the thematic mapper instrument, comp...
In this paper the support system interference on the zero lift drag of an axisymmetric and an aircra...
A Boltz body of revolution (fineness ratio 7.5:1) was tested in the Southampton University Magnetic ...
The reuseable exterior insulation system (REI) is studied to determine the optimal reentry trajector...