Author: Thomas G. Gainer
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 148
Book Description
Summary of Transformation Equations and Equations of Motion Used in Free Flight and Wind Tunnel Data Reduction and Analysis
Author: Thomas G. Gainer
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 140
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 140
Book Description
Summary of Transformation Equations and Equations of Motion Used in Free-flight and Wind-tunnel Data Reduction and Analysis
Author: Thomas G. Gainer
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 148
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 148
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Book Description
Stability and Control Estimation Flight Test Results for the SR-71 Aircraft With Externally Mounted Experiments
Author: Timothy R. Moes
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
A maximum-likelihood output-error parameter estimation technique is used to obtain stability and control derivatives for the NASA Dryden Flight Research Center SR-71A airplane and for configurations that include experiments externally mounted to the top of the fuselage. This research is being done as part of the envelope clearance for the new experiment configurations. Flight data are obtained at speeds ranging from Mach 0.4 to Mach 3.0, with an extensive amount of test points at approximately Mach 1.0. Pilot-input pitch and yaw-roll doublets are used to obtain the data. This report defines the parameter estimation technique used, presents stability and control derivative results, and compares the derivatives for the three configurations tested. The experimental configurations studied generally show acceptable stability, control, trim, and handling qualities throughout the Mach regimes tested.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
A maximum-likelihood output-error parameter estimation technique is used to obtain stability and control derivatives for the NASA Dryden Flight Research Center SR-71A airplane and for configurations that include experiments externally mounted to the top of the fuselage. This research is being done as part of the envelope clearance for the new experiment configurations. Flight data are obtained at speeds ranging from Mach 0.4 to Mach 3.0, with an extensive amount of test points at approximately Mach 1.0. Pilot-input pitch and yaw-roll doublets are used to obtain the data. This report defines the parameter estimation technique used, presents stability and control derivative results, and compares the derivatives for the three configurations tested. The experimental configurations studied generally show acceptable stability, control, trim, and handling qualities throughout the Mach regimes tested.
Comparison of Wind Velocity in Thunderstorms Determined from Measurements by a Ground-based Doppler Radar and an F-106B Airplane
Author: J. W. Usry
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aeronautics in meteorology
Languages : en
Pages : 44
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 42
Book Description
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 380
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 380
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
Book Description
NASA Reference Publication
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 636
Book Description