Experience has shown that the determination of the take-off and. landing characteristics of airplanes requires specialized, equipment of a high degree of precision and reliability and demands great care in the evaluation and interpretation of data. It is believed, therefore, that a description of the apparatus and methods that have been developed by the NACA for these measurements might be of considerable interest, particularly to flight-test groups that have had little experience with landing and. take-off measurements. The basic principles and essential details of the Committee's equipment are described, the methods of utilizing the apparatus and of reducing the data are explained, and sample test results are presented
The main aim is to describe a series of flying qualities investigations designed to look at flying q...
This note contains photos and descriptions of airplane flight apparatus for use in conjunction with ...
The measurement of total airplane drag in flight is necesssry to assess the applicability of wind-tu...
This report covers the results of an investigation carried on at the Langley Memorial Aeronautical L...
In order to determine the first part of the flight path a new method is described which requires onl...
The overall errors of the service altimeter installations of a variety of civil transport, military,...
A method for evaluating aircraft takeoff performance from brake release to air-phase height that req...
The characteristics of a proposed acceleration-type take-off indicator were observed during take-off...
This investigation was made for the purpose of obtaining information on the maneuverability of the F...
"The overall errors of the service altimeter installations of a variety of civil transport, military...
The object of this report is the description of a method which seems to be practicable for determini...
Report presents the results of an investigation to determine the character and importance of the tra...
An investigation was undertaken to determine the character and importance of the transition phase be...
The object of this report is the description of a method which seems to be practicable for determini...
The design of and the experience with an inexpensive, hand-portable, onboard data system used to rec...
The main aim is to describe a series of flying qualities investigations designed to look at flying q...
This note contains photos and descriptions of airplane flight apparatus for use in conjunction with ...
The measurement of total airplane drag in flight is necesssry to assess the applicability of wind-tu...
This report covers the results of an investigation carried on at the Langley Memorial Aeronautical L...
In order to determine the first part of the flight path a new method is described which requires onl...
The overall errors of the service altimeter installations of a variety of civil transport, military,...
A method for evaluating aircraft takeoff performance from brake release to air-phase height that req...
The characteristics of a proposed acceleration-type take-off indicator were observed during take-off...
This investigation was made for the purpose of obtaining information on the maneuverability of the F...
"The overall errors of the service altimeter installations of a variety of civil transport, military...
The object of this report is the description of a method which seems to be practicable for determini...
Report presents the results of an investigation to determine the character and importance of the tra...
An investigation was undertaken to determine the character and importance of the transition phase be...
The object of this report is the description of a method which seems to be practicable for determini...
The design of and the experience with an inexpensive, hand-portable, onboard data system used to rec...
The main aim is to describe a series of flying qualities investigations designed to look at flying q...
This note contains photos and descriptions of airplane flight apparatus for use in conjunction with ...
The measurement of total airplane drag in flight is necesssry to assess the applicability of wind-tu...