Add to ORKGStatistical measurements of contact conditions have been obtained, by means of a special photographic technique, of 478 landings of present-day transport airplanes made during routine daylight operations in clear air at the Washington National Airport. From the measurements, sinking speeds, rolling velocities, bank angles, and horizontal speeds at the instant before contact have been evaluated and a limited statistical analysis of the results has been made and is reported in this report
Some loading conditions imposed during ground turning maneuvers are presented for arrival and depart...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
This report describes flight and landing tests made on a group of conventional airplanes. The upward...
Statistical measurements of contact conditions have been obtained by means of a specially built moti...
Statistical measurements of contact conditions have been obtained, by means of a special photographi...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
The National Aeronautics and Space Administration has recently completed a statistical investigation...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
The sources of error that may enter into the measurement of airspeed by pitot-static methods are rev...
An in-flight evaluation of transport roll characteristics in the landing approach was made with a ge...
Utilization of delta-wing interceptor aircraft in evaluation of low lift-drag ratios on approach and...
Stability and control characteristics determined from tests in the Langley 19-foot pressure tunnel o...
This report presents the results of maneuverability tests of an O3U-1 observation airplane. This inv...
Velocity, gust, and height data analysis from four-engine turbojet transport airplan
Some loading conditions imposed during ground turning maneuvers are presented for arrival and depart...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
This report describes flight and landing tests made on a group of conventional airplanes. The upward...
Statistical measurements of contact conditions have been obtained by means of a specially built moti...
Statistical measurements of contact conditions have been obtained, by means of a special photographi...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
The National Aeronautics and Space Administration has recently completed a statistical investigation...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Flight tests were made to determine the profile-drag coefficients of a portion of the original wing ...
The sources of error that may enter into the measurement of airspeed by pitot-static methods are rev...
An in-flight evaluation of transport roll characteristics in the landing approach was made with a ge...
Utilization of delta-wing interceptor aircraft in evaluation of low lift-drag ratios on approach and...
Stability and control characteristics determined from tests in the Langley 19-foot pressure tunnel o...
This report presents the results of maneuverability tests of an O3U-1 observation airplane. This inv...
Velocity, gust, and height data analysis from four-engine turbojet transport airplan
Some loading conditions imposed during ground turning maneuvers are presented for arrival and depart...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
This report describes flight and landing tests made on a group of conventional airplanes. The upward...