Add to ORKGPilot performance of landing maneuver in T-33-A jet trainer with restricted fields of vie
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Friction coefficients and wear characteristics for X-15 aircraft skid landing gea
Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during lan...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
The approach and flare maneuvers for the first 30 flights of the X-15 airplane and the various contr...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Theoretical dynamic analysis of landing loads on vehicle with tricycle landing gear compared with X-...
Performance characteristics of data acquisition flight test sensors used on X-15 aircraf
Simple model describing final airborne stages of landing transport aircraft manuall
The first landing of the X-15 airplane was made at 8:43 a.m., June 8, 1959, on the hard surface of R...
Utilization of delta-wing interceptor aircraft in evaluation of low lift-drag ratios on approach and...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Statistical analysis of normal load factor just prior to touchdown for light aircraf
Pilot performance of landing maneuver in T-33-A jet trainer with restricted fields of vie
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Friction coefficients and wear characteristics for X-15 aircraft skid landing gea
Measurements of loads, accelerations, and displacements of x-15 aircraft and landing gear during lan...
The landing contact conditions for the HL-10, M2-F2/F3, and the X-24A lifting body vehicles are anal...
The approach and flare maneuvers for the first 30 flights of the X-15 airplane and the various contr...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Theoretical dynamic analysis of landing loads on vehicle with tricycle landing gear compared with X-...
Performance characteristics of data acquisition flight test sensors used on X-15 aircraf
Simple model describing final airborne stages of landing transport aircraft manuall
The first landing of the X-15 airplane was made at 8:43 a.m., June 8, 1959, on the hard surface of R...
Utilization of delta-wing interceptor aircraft in evaluation of low lift-drag ratios on approach and...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Drag characteristics have been obtained for the X-15 airplane during unpowered flight. These data re...
Statistical analysis of normal load factor just prior to touchdown for light aircraf
Pilot performance of landing maneuver in T-33-A jet trainer with restricted fields of vie
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Friction coefficients and wear characteristics for X-15 aircraft skid landing gea