Author: Publisher:
ISBN:
Category : Transport planes
Languages : en
Pages : 160
Book Description
Operational Experiences of Turbine-powered Commercial Transport Airplanes
Author: Operational Experiences of Turbine-powered Commercial Transport Airplanes
Author: Langley Airworthiness BranchPublisher:
ISBN:
Category :
Languages : en
Pages : 151
Book Description
Airspeed Operating Practices of Turbine-powered Commercial Transport Airplanes
Author: Thomas L. ColemanPublisher:
ISBN:
Category : Air speed
Languages : en
Pages : 32
Book Description
Airspeed Operating Practices of Turbine-Powered Commercial Transport Airplanes
Author: Thomas L. ColemanSummary of V-G Data Obtained from Turbine-powered Transport Airplanes from 1959 to 1963
Author: Walter G. WalkerPublisher:
ISBN:
Category : Acceleration (Mechanics)
Languages : en
Pages : 28
Book Description
NASA Technical Note
Author: Statistical Analysis of Landing-contact Conditions for the XB-70 Airplane
Author: Ronald J. WilsonPublisher:
ISBN:
Category : B-70 bomber
Languages : en
Pages : 36
Book Description
An Investigation of Landing-contact Conditions for Several Turbojet Transports During Routine Daylight Operations at New York International Airport
Author: Joseph W. SticklePublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Book Description
A Piloted Simulator Investigation of Ground Effect on the Landing Maneuver of a Large, Tailless, Delta-wing Airplane
Author: C. Thomas SnyderPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60
Book Description
The influence of ground effect on the landing flare characteristics of a supersonic transport airplane (SST) was investigated in a fixed cockpit simulator. Simulations of an ogee-modified delta-wing F5D-1 airplane and a subsonic jet transport were used for evaluating the simulator and as a reference configurations during landing comparisons. Dynamic responses of the SST to seven different ground-effect models during controls-fixed and constant-attitude descents are also presented, followed by piloted subjective assessments. A summary of ground effects on delta-like wings is included in the appendixes.
Some Effects of Flight Path and Atmospheric Variations on the Boom Propagated from a Supersonic Aircraft
Author: Raymond L. BargerPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40
Book Description
Equations for the shock wave envelope and cusp line associated with the boom propagated from a supersonic aircraft are formulated in terms of the moving-trihedral coordinate system for flight in a uniform atmosphere and also in an atmosphere with a linear sound-speed gradient. Ray-tube theory is used to calculate the lateral distribution of boom intensity in an atmosphere with a linear sound-speed gradient and also to investigate the effect of a general wind and sound-speed gradient on the ground-track intensity. The relative effects of wind and temperature gradient are treated. The mechanism of focusing by winds and by ground structures are discussed qualitatively.