Add to ORKGA wind-tunnel investigation has been made to determine the characteristics of external-flow jet-augmented double slotted flaps which appear suitable for application to airplanes with pod-mounted engines. The investigation included tests of the rectangular wing with an aspect ratio of 6 over a momentum-coefficient range from 0 to 28. Lift coefficients larger than the jet reaction in the lift direction were obtained with the external-flow jet-augmented double slotted flaps
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
An investigation of a full-span 17-percent-chord internal-flow jet-augmented flap on an aspect-ratio...
An investigation was made in the 5.18 m (17 ft) test section of the Langley 300 MPH 7 by 10 foot tun...
A wind-tunnel investigation at low speeds has been made to study the aerodynamic characteristics of ...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
Wind tunnel investigation of external-flow jet-flap transport configuration having full-span tripple...
Wind tunnel tests of large jet transport aircraft model with external flow jet fla
A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...
Wind tunnel investigation of jet transport airplane configuration with external flow jet flap and in...
A wind-tunnel investigation has been conducted to determine the performance and static stability and...
An investigation has been conducted to determine the aerodynamic characteristics of a large-scale su...
Wind tunnel tests of swept wing jet transport aircraft model with four pod mounted engines under win...
An investigation was made in the LMAL 7- by 10-foot wind tunnel of a NACA 23021 airfoil with a doubl...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
An investigation of a full-span 17-percent-chord internal-flow jet-augmented flap on an aspect-ratio...
An investigation was made in the 5.18 m (17 ft) test section of the Langley 300 MPH 7 by 10 foot tun...
A wind-tunnel investigation at low speeds has been made to study the aerodynamic characteristics of ...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
Wind tunnel investigation of external-flow jet-flap transport configuration having full-span tripple...
Wind tunnel tests of large jet transport aircraft model with external flow jet fla
A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...
Wind tunnel investigation of jet transport airplane configuration with external flow jet flap and in...
A wind-tunnel investigation has been conducted to determine the performance and static stability and...
An investigation has been conducted to determine the aerodynamic characteristics of a large-scale su...
Wind tunnel tests of swept wing jet transport aircraft model with four pod mounted engines under win...
An investigation was made in the LMAL 7- by 10-foot wind tunnel of a NACA 23021 airfoil with a doubl...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
An investigation has been conducted in a full-scale tunnel to determine the effects of variations in...
An investigation of a full-span 17-percent-chord internal-flow jet-augmented flap on an aspect-ratio...
An investigation was made in the 5.18 m (17 ft) test section of the Langley 300 MPH 7 by 10 foot tun...