Available information on weight and inertia, aerodynamic derivatives, control characteristics, and stability augmentation systems is documented for 10 representative contemporary airplanes. Data sources are given for each airplane. Flight envelopes are presented and dimensional derivatives, transfer functions for control inputs, and several selected handling qualities parameters have been computed and are tabulated for 10 different flight conditions including the power approach configuration. The airplanes documented are the NT-33A, F-104A, F-4C, X-15, HL-10, Jetstar, CV-880M, B-747, C-5A, and XB-70A
This report outlines the flight conditions that are usually critical in determining the design of co...
The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Har...
Report discusses the results of an analysis of available data to determine what measured characteris...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
The handling qualities of the YF-12 airplane as observed during NASA research flights over the past ...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
Transfer functions of pilot for determining longitudinal aircraft controllability and pilot performa...
The notion of airplane stability and control being a balancing act between stability and control ha...
This volume contains a delineation of fundamental and mechanization-specific flight control characte...
Initial envelope clearance and subsequent flight testing of a new, fully augmented airplane with an ...
The stability and control characteristics of the XB-70 airplane were evaluated for Mach numbers up t...
The magnitude and frequency of occurrence of aircraft responses and control inputs during 27 flights...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
This report outlines the flight conditions that are usually critical in determining the design of co...
The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Har...
Report discusses the results of an analysis of available data to determine what measured characteris...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
The handling qualities of the YF-12 airplane as observed during NASA research flights over the past ...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
A flight-test program was conducted to determine the effect of advanced flight control systems and d...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
Transfer functions of pilot for determining longitudinal aircraft controllability and pilot performa...
The notion of airplane stability and control being a balancing act between stability and control ha...
This volume contains a delineation of fundamental and mechanization-specific flight control characte...
Initial envelope clearance and subsequent flight testing of a new, fully augmented airplane with an ...
The stability and control characteristics of the XB-70 airplane were evaluated for Mach numbers up t...
The magnitude and frequency of occurrence of aircraft responses and control inputs during 27 flights...
A TF-8A airplane was equipped with a transport type supercritical wing and fuselage fairings to eval...
This report outlines the flight conditions that are usually critical in determining the design of co...
The handling qualities of the F-8 digital fly by wire airplane are evaluated by using the Cooper-Har...
Report discusses the results of an analysis of available data to determine what measured characteris...