The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are analyzed statistically for 81 landings. The landing contact parameters analyzed are true airspeed, peak normal acceleration at the center of gravity, roll angle, and roll velocity. Ground measurement parameters analyzed are lateral and longitudinal distance from intended touchdown, lateral distance from touchdown to full stop, and rollout distance. The results are presented in the form of histograms for frequency distributions and cumulative frequency distribution probability curves with a Pearson Type 3 curve fit for extrapolation purposes
An in-flight evaluation of transport roll characteristics in the landing approach was made with a ge...
Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during lan...
The main aim is to describe a series of flying qualities investigations designed to look at flying q...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
Statistical analysis of landing contact conditions and slideout distances of X-15 research airplan
The National Aeronautics and Space Administration has recently completed a statistical investigation...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
Statistical analysis of normal load factor just prior to touchdown for light aircraf
This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...
A series of landings was performed with a straight-wing airplane to evaluate the effect of low lift-...
A broad survey of possible orbiter landing configurations was made with specific goals of defining b...
A flight evaluation was made of the mechanical hydraulic flight control system and the electrohydrau...
An experimental study was conducted in order to determine the landing-impact behavior of a 0.3-scale...
Statistical measurements of contact conditions have been obtained by means of a specially built moti...
Performance characteristics during landing approach of large powered-lift jet transpor
An in-flight evaluation of transport roll characteristics in the landing approach was made with a ge...
Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during lan...
The main aim is to describe a series of flying qualities investigations designed to look at flying q...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
Statistical analysis of landing contact conditions and slideout distances of X-15 research airplan
The National Aeronautics and Space Administration has recently completed a statistical investigation...
Percentage distributions of 423 pilot ratings obtained from 27 flights are used to indicate the gene...
Statistical analysis of normal load factor just prior to touchdown for light aircraf
This paper examines flight-measured subsonic lift and drag characteristics of seven lifting-body and...
A series of landings was performed with a straight-wing airplane to evaluate the effect of low lift-...
A broad survey of possible orbiter landing configurations was made with specific goals of defining b...
A flight evaluation was made of the mechanical hydraulic flight control system and the electrohydrau...
An experimental study was conducted in order to determine the landing-impact behavior of a 0.3-scale...
Statistical measurements of contact conditions have been obtained by means of a specially built moti...
Performance characteristics during landing approach of large powered-lift jet transpor
An in-flight evaluation of transport roll characteristics in the landing approach was made with a ge...
Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during lan...
The main aim is to describe a series of flying qualities investigations designed to look at flying q...