The analysis of results of wind-tunnel stability and control tests of powered airplane models in terms of the flying qualities of full-scale airplanes is advocated. In order to indicated the topics upon which comments are considered desirable in the report of a wind-tunnel stability and control investigation and to demonstrate the nature of the suggested analysis, the present NACA flying-qualities requirements are discussed in relation to wind-tunnel tests. General procedures for the estimation of flying qualities from wind-tunnel tests are outlined
The effects of power on the stability and the control characteristics of an airplane are discussed a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
This report outlines the flight conditions that are usually critical in determining the design of co...
The material given in this report summarizes some of the results of recent research that will aid th...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The National Advisory Committee for Aeronautics is undertaking an investigation of the flying qualit...
Report discusses the results of an analysis of available data to determine what measured characteris...
Results are presented for a series of tests made by the Advisory Committee's staff at Langley Field ...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
Low Mach number longitudinal-stability and control characteristics as predicted by use of wind tunne...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
Here, it is shown that the construction of an airplane model can and should be simplified in order t...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
This report outlines the flight conditions that are usually critical in determining the design of co...
The material given in this report summarizes some of the results of recent research that will aid th...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
The National Advisory Committee for Aeronautics is undertaking an investigation of the flying qualit...
Report discusses the results of an analysis of available data to determine what measured characteris...
Results are presented for a series of tests made by the Advisory Committee's staff at Langley Field ...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
The stability of an airplane can be easily determined by wind-tunnel tests, especially by simple tes...
Low Mach number longitudinal-stability and control characteristics as predicted by use of wind tunne...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
Here, it is shown that the construction of an airplane model can and should be simplified in order t...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...