This report describes work carried out at The College of Aeronautics, Cranfield, during the first year of a contract to study the effects of atmospheric turbulence on the M.S.76O % Paris' aircraft. The aircraft was fitted with an instrumentation system capable of recording ten aircraft quantities, the data being stored on magnetic tape. From data recorded during flight tests, transfer functions for symmetric acceleration responses of the aircraft to turbulence may be obtained. Also, transfer functions may be determined for symmetric tailplane loads in turbulence, including the effect of the downwash from the wing elastic modes, and the tailplane elastic dynamic response. The report contains detailed static and dynamic performance ...
This study deals with the problem of turbulence measurement with small remotely piloted aircraft (...
Advanced methods were developed to determine time varying winds and turbulence from digital flight d...
An analytical study has been made to assess the loads developed on the horizontal tail of an autopil...
A turbulence response investigation was conducted with the XB-70 airplane. No special turbulence pen...
After an incident which, it was suspected, was due to symmetric elevator flutter, had occurred on t...
A method of obtaining aircraft frequency-response from transient response data by Fourier analysis ...
Various types of atmospheric turbulence measurements are addressed for the purpose of stimulating di...
A flight instrumentation system for the acquisition of atmospheric turbulence data is described. Air...
The computed RMS and peak responses due to atmospheric turbulence and discrete wind shears, respecti...
Calculated responses of symmetrical airplane motions, wing deformations, and wing loads due to conti...
15th MST Radar WorkshopSession M4: MST Radar scattering, turbulence and small-scale processesMay 30 ...
PDFTech ReportDOT-TSC-FAA-72-38, SupFAA-RD-73-20, SupplementRemote sensingAtmospheric turbulenceClea...
Thesis (Sc.D.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1950.Vita. ...
The effects of 2.5-m/sec vertical gusts on the flight characteristics of a 1:8.6 scale model of a Mi...
For a 2-week period in the spring of 1977, data were collected onboard wide-body jet transports for ...
This study deals with the problem of turbulence measurement with small remotely piloted aircraft (...
Advanced methods were developed to determine time varying winds and turbulence from digital flight d...
An analytical study has been made to assess the loads developed on the horizontal tail of an autopil...
A turbulence response investigation was conducted with the XB-70 airplane. No special turbulence pen...
After an incident which, it was suspected, was due to symmetric elevator flutter, had occurred on t...
A method of obtaining aircraft frequency-response from transient response data by Fourier analysis ...
Various types of atmospheric turbulence measurements are addressed for the purpose of stimulating di...
A flight instrumentation system for the acquisition of atmospheric turbulence data is described. Air...
The computed RMS and peak responses due to atmospheric turbulence and discrete wind shears, respecti...
Calculated responses of symmetrical airplane motions, wing deformations, and wing loads due to conti...
15th MST Radar WorkshopSession M4: MST Radar scattering, turbulence and small-scale processesMay 30 ...
PDFTech ReportDOT-TSC-FAA-72-38, SupFAA-RD-73-20, SupplementRemote sensingAtmospheric turbulenceClea...
Thesis (Sc.D.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1950.Vita. ...
The effects of 2.5-m/sec vertical gusts on the flight characteristics of a 1:8.6 scale model of a Mi...
For a 2-week period in the spring of 1977, data were collected onboard wide-body jet transports for ...
This study deals with the problem of turbulence measurement with small remotely piloted aircraft (...
Advanced methods were developed to determine time varying winds and turbulence from digital flight d...
An analytical study has been made to assess the loads developed on the horizontal tail of an autopil...