An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler direct lift control system. Slot spoilers are believed to have advantages over flap-type direct lift control (DLC) systems because of the small amount of power required for actuation. These tests, run at a Reynolds number of 1,400,000 showed that up to 78 percent of the lift due to flap deflection could be spoiled by opening several spanwise slots within the flaps. For a given lift change the drag change was significantly less than that which would be obtained by a variable flap DLC system. A nozzle-shaped slot was the most effective of the slot shapes tested.Prepared at Langley Research Center.N72-13978.Includes bibliographical references (p...
This report presents the results of an investigation to determine the effect of boundary layer contr...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation has been conducted in the Langley 19-foot pressure tunnel to determine the maximum ...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
A wind-tunnel investigation has been conducted to determine the effects of slot spoilers on the long...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
A wind-tunnel investigation has been conducted to determine the performance and static stability and...
Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
An exteneire inrtwtigation wag made in the NACA 7- by 10~oot wind iunmd of Epoiler, dejector, and id...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
An experimental study has been carried out on an airfoil with slotted flap and spoiler using Joukows...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
This report presents the results of an investigation to determine the effect of boundary layer contr...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation has been conducted in the Langley 19-foot pressure tunnel to determine the maximum ...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
A wind-tunnel investigation has been conducted to determine the effects of slot spoilers on the long...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Analysis indicates that this use of spoiler ailerons is feasible and desirable for normal emergency ...
A wind-tunnel investigation has been conducted to determine the performance and static stability and...
Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet
An investigation was made in the NACA 7 by 10 foot wind tunnel to find the increase in maximum lift ...
An exteneire inrtwtigation wag made in the NACA 7- by 10~oot wind iunmd of Epoiler, dejector, and id...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
An experimental study has been carried out on an airfoil with slotted flap and spoiler using Joukows...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
This report presents the results of an investigation to determine the effect of boundary layer contr...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation has been conducted in the Langley 19-foot pressure tunnel to determine the maximum ...