Add to ORKGThe paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. 37974) research airplane. Data are presented for a range of calibrated airspeed from 167 miles per hour to 474 miles per hour
This report contains the flight-test results of the lateral and directional-stability and control ph...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...
The aerodynamic and mass factors governing lateral stability are discussed and formulas are given fo...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
This report contains the flight-test results of the lateral and directional-stability and control ph...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
Flight tests were made of the flying qualities of an F-47D-30 airplane to determine the longitudinal...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
This report contains the flight-test results of the lateral and directional-stability and control ph...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...
The aerodynamic and mass factors governing lateral stability are discussed and formulas are given fo...
The paper presents flight measurements of the dynamic lateral stability of the D-558-II (BuAero No. ...
This report contains the flight-test results of the lateral and directional-stability and control ph...
In connection with the DVL Report 272 on the theory of the lateral stability of airplanes, the forma...
Measurements have been made of the stability characteristics of the D-558-1 airplane in steadily inc...
Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like conf...
Flight tests were made of the flying qualities of an F-47D-30 airplane to determine the longitudinal...
Contains a few measurements of the variation of elevator angle and elevator force with Mach number a...
This report contains the flight-test results of the lateral and directional-stability and control ph...
The determination of lateral stability derivatives for a navion airplane from steady state dynamic f...
The aerodynamic and mass factors governing lateral stability are discussed and formulas are given fo...