Author: James A. Weiberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Comparisons with the results of tests on the same model but having a combination slot suction and blowing boundary-layer-control system (Arado) on the trailing-edge flaps and ailerons indicated considerably lower suction flow requirements for the area-suction flaps.
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Area-suction Flaps
Author: James A. Weiberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Comparisons with the results of tests on the same model but having a combination slot suction and blowing boundary-layer-control system (Arado) on the trailing-edge flaps and ailerons indicated considerably lower suction flow requirements for the area-suction flaps.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Comparisons with the results of tests on the same model but having a combination slot suction and blowing boundary-layer-control system (Arado) on the trailing-edge flaps and ailerons indicated considerably lower suction flow requirements for the area-suction flaps.
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Blowing Flaps
Author: Roy N. Griffin
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps
Author: James A. Weiberg
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Large Scale Wind-tunnel Tests of Airplane Model with Unswept, Aspect-ratio-10 Wing, 2 Propellers, and Blowing Flaps [with List of References]
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 47
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 408
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 408
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 690
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 690
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1300
Book Description
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1300
Book Description
Simplified Method for Determination of Critical Height of Distributed Roughness for Boundary-layer Transition at Mach Numbers from 0 to 5
Author: Albert L. Braslow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 624
Book Description
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
A Flight Examination of Operating Problems of V/STOL Aircraft in STOL Type Landing and Approach
Author: Robert C. Innis
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description