Add to ORKGAn experimental and analytical investigation was conducted to determine which characteristics of a l...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Performance characteristics of data acquisition flight test sensors used on X-15 aircraf
The first landing of the X-15 airplane was made at 8:43 a.m., June 8, 1959, on the hard surface of R...
Statistical analysis of landing contact conditions and slideout distances of X-15 research airplan
Theoretical dynamic analysis of landing loads on vehicle with tricycle landing gear compared with X-...
The approach and flare maneuvers for the first 30 flights of the X-15 airplane and the various contr...
During the first powered flight of the North American X-15 research airplane on September 17, 1959, ...
X-15 aircraft handling qualities and longitudinal stability and control during launch, climbout, sem...
Friction coefficients and wear characteristics for X-15 aircraft skid landing gea
Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...
Aerodynamic lift and drag characteristics comparison between full scale and wind tunnel model of X-1...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...
Tricycle skid-type landing gear system - equations of motion for x-15 vehicle slideout dynamic
An experimental and analytical investigation was conducted to determine which characteristics of a l...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Performance characteristics of data acquisition flight test sensors used on X-15 aircraf
The first landing of the X-15 airplane was made at 8:43 a.m., June 8, 1959, on the hard surface of R...
Statistical analysis of landing contact conditions and slideout distances of X-15 research airplan
Theoretical dynamic analysis of landing loads on vehicle with tricycle landing gear compared with X-...
The approach and flare maneuvers for the first 30 flights of the X-15 airplane and the various contr...
During the first powered flight of the North American X-15 research airplane on September 17, 1959, ...
X-15 aircraft handling qualities and longitudinal stability and control during launch, climbout, sem...
Friction coefficients and wear characteristics for X-15 aircraft skid landing gea
Base pressure measurements have been made on the fuselage, 10 deg.-wedge vertical fin, and side fair...
Aerodynamic lift and drag characteristics comparison between full scale and wind tunnel model of X-1...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Flight test data on longitudinal, lateral, and directional stability and control derivatives of X-15...
Tricycle skid-type landing gear system - equations of motion for x-15 vehicle slideout dynamic
An experimental and analytical investigation was conducted to determine which characteristics of a l...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Performance characteristics of data acquisition flight test sensors used on X-15 aircraf