Add to ORKGReport presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel of spoiler, deflector, and slot types of lateral-control device on wings with full-span split and slotted flaps. The static rolling and yawing moments were determined for all the devices tested, and the static hinge moments and the time response were determined for a few devices of each type
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Tests of a partial-span model of a large bomber-type air1ane\ud were conducted to determine the. aer...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determi...
An exteneire inrtwtigation wag made in the NACA 7- by 10~oot wind iunmd of Epoiler, dejector, and id...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
An investigation of the undesirable delayed action, or lag, of the spoiler-type lateral control devi...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
This report covers the fifth of a series of systematic investigations in which lateral control devic...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
This report presents the results of wind tunnel tests to determine the effectiveness of various meth...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Tests of a partial-span model of a large bomber-type air1ane\ud were conducted to determine the. aer...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determi...
An exteneire inrtwtigation wag made in the NACA 7- by 10~oot wind iunmd of Epoiler, dejector, and id...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
An investigation of the undesirable delayed action, or lag, of the spoiler-type lateral control devi...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
This report covers the fifth of a series of systematic investigations in which lateral control devic...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
This report presents the results of wind tunnel tests to determine the effectiveness of various meth...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
Tests of a partial-span model of a large bomber-type air1ane\ud were conducted to determine the. aer...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determi...