Add to ORKGTests were made on the 1927 Williams racer in order to determine the effect of the wing radiator on the airfoil characteristics. It was found that the radiator doubled the minimum drag of the portion of the wing it covered, and also reduced the lift somewhat
The N.A.C.A. has conducted tests to provide more complete data than were previously available for es...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
At the request of the Army Air Corps tests were conducted on a mock-up of the YO-31A airplane to det...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of a large...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
This report contains a survey of past radiator research. This report also is intended as a systemati...
This reports combines the wind tunnel results of radiator tests made at the Navy Aerodynamical Labor...
The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various com...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This report contains the results of a series of tests with three wing models. By changing the sectio...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
The N.A.C.A. has conducted tests to provide more complete data than were previously available for es...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
At the request of the Army Air Corps tests were conducted on a mock-up of the YO-31A airplane to det...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of a large...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
This report contains a survey of past radiator research. This report also is intended as a systemati...
This reports combines the wind tunnel results of radiator tests made at the Navy Aerodynamical Labor...
The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various com...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
This report contains the results of a series of tests with three wing models. By changing the sectio...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
This report gives the full-scale aerodynamic characteristics of five different aluminum alloy propel...
The N.A.C.A. has conducted tests to provide more complete data than were previously available for es...
Aerodynamic effects of airfoil thickness on transonic flutter characteristics of swept and unswept w...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...