The handling qualities of the YF-12 airplane as observed during NASA research flights over the past five years were reviewed. Aircraft behavior during takeoff, acceleration, climb, cruise, descent, and landing are discussed. Pilot comments on the various flight phases and tasks are presented. Handling qualities parameters such as period, damping, amplitude ratios, roll-yaw coupling, and flight path response sensitivity are compared to existing and proposed handling qualities criteria. The influence of the propulsion systems, stability augmentation, autopilot systems, atmospheric gusts, and temperature changes are also discussed. YF-12 experience correlates well with flying qualities criteria, except for longitudinal short period damping, wh...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
X-15 aircraft handling qualities and longitudinal stability and control during launch, climbout, sem...
A flying qualities evaluation conducted on the YF-17 airplane permitted assessment of its precision ...
Approximately 25 years ago NASA Dryden Flight Research Center, Edwards, California, initiated the ev...
A piloted simulation study was conducted with the aim of advancing the development of longitudinal h...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
The objectives and status of the propulsion program, along with the results acquired in the various ...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
A true gust velocity measuring system designed to alleviate complications resulting from airframe fl...
Available information on weight and inertia, aerodynamic derivatives, control characteristics, and s...
At Mach numbers of approximately 3.0 and altitudes greater than 21,300 meters, the original altitude...
The history of NASA's interest in supersonic research and the agency's contribution to the developme...
The stability and control characteristics of the XB-70 airplane were evaluated for Mach numbers up t...
Flight tests were conducted with the YF-12 airplane to examine the airplane's longitudinal character...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
X-15 aircraft handling qualities and longitudinal stability and control during launch, climbout, sem...
A flying qualities evaluation conducted on the YF-17 airplane permitted assessment of its precision ...
Approximately 25 years ago NASA Dryden Flight Research Center, Edwards, California, initiated the ev...
A piloted simulation study was conducted with the aim of advancing the development of longitudinal h...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
The objectives and status of the propulsion program, along with the results acquired in the various ...
Flight test to determine flying qualities and dynamic stability derivatives of supersonic fighter ai...
A true gust velocity measuring system designed to alleviate complications resulting from airframe fl...
Available information on weight and inertia, aerodynamic derivatives, control characteristics, and s...
At Mach numbers of approximately 3.0 and altitudes greater than 21,300 meters, the original altitude...
The history of NASA's interest in supersonic research and the agency's contribution to the developme...
The stability and control characteristics of the XB-70 airplane were evaluated for Mach numbers up t...
Flight tests were conducted with the YF-12 airplane to examine the airplane's longitudinal character...
The flying qualities of the CV-990 jet transport were evaluated over the normal operating flight env...
The handling qualities of the F-8 digital fly-by-wire airplane are evaluated by using the Cooper-Har...
X-15 aircraft handling qualities and longitudinal stability and control during launch, climbout, sem...
A flying qualities evaluation conducted on the YF-17 airplane permitted assessment of its precision ...