A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps

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A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 2001

A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Aerodynamics categories.

An improved semiempirical method has been developed to estimate the static aerodynamics of configurations that use a trailing edge flap for control. The method is based on deflecting the full aft-located lifting surface an amount that allows the normal force coefficient to be equal to that generated by the deflected flap. A transfer in pitching moments and a modified axial force coefficient is arrived to complete the set of static aerodynamics . The method to give satisfactory results over the practical range that trailing edge flaps are contemplated for use. However, additional wind tunnel data is needed to refine and expand the applicability of the method. This is particularly true for transonic Mach numbers and for supersonic Mach numbers where the angle of attack and control deflection are of the same.

A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 2001

A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Aerodynamics categories.

An improved semiempirical method has been developed to estimate the static aerodynamics of configurations that use a trailing edge flap for control. The method is based on deflecting the full aft-located lifting surface an amount that allows the normal force coefficient to be equal to that generated by the deflected flap. A transfer in pitching moments and a modified axial force coefficient is arrived to complete the set of static aerodynamics . The method to give satisfactory results over the practical range that trailing edge flaps are contemplated for use. However, additional wind tunnel data is needed to refine and expand the applicability of the method. This is particularly true for transonic Mach numbers and for supersonic Mach numbers where the angle of attack and control deflection are of the same.

A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps

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Author :
language : en
Publisher:
Release Date : 2001

A Semiempirical Method For Predicting Aerodynamics Of Trailing Edge Flaps written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with categories.

An Improved Semi empirical Method has been developed to estimate the static aerodynamics of configurations that use a trailing edge flap for control. The method is based on deflecting the full aft-located lifting surface an amount that allows the normal force coefficient to be equal to that generated by the deflected flap. A transfer in pitching moments and a modified axial force coefficient is derived to complete the set of static aerodynamics. The method is derived using theoretical methods that are a part of the 1998 version of the Naval Surface Warfare Center aeroprediction code and two sets of experimental data. Comparison of the improved method to available data shows the method to give satisfactory results over the practical range that trailing edge flaps are contemplated for use. However, additional wind tunnel data is needed to refine and expand the applicability of the method. This is particularly true for transonic Mach numbers and for supersonic Mach numbers where the angle of attack and control deflection are of the same sign.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1994

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.

The 2002 Version Of The Aeroprediction Code

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 2002

The 2002 Version Of The Aeroprediction Code written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aerodynamics categories.

A new version of the aeroprediction code (APC), the AP02, has been developed to address the requirements arising from advanced weapon concepts. The AP02 was formed by adding significant new technology and several productivity improvements to the previous version of the APC, the AP98. New technology added included 6 and 8 fin aerodynamics, improved nonlinear aerodynamics, improved pitch damping predictions, improved power-on base drag estimates, base-bleed effect on base drag estimation, improved axial force of nonaxisymmetric bodies and trailing-edge flap capability. Other improvements and productivity enhancements include an aerodynamic smoother, ballistic and three degree-of-freedom simulation modules as well as refinements for the pre- and post-processor for inputs and outputs of the AP02. Comparison of the predicted aerodynamics of the AP02 to AP98 and experimental data showed the AP02 to be slightly better than the AP98 in most cases that both codes would handle. However, due to the additional new technology incorporated into the AP02, many new options are available in the AP02 that are not available in the AP98. Therefore, the AP02 is more robust and, on average, is slightly more accurate than the AP98 in predicting aerodynamics of weapons.

An Engineering Method For Estimating The Aerodynamic Characteristics Of Circulation Control Wings Ccw

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Author : Campbell Henderson
language : en
Publisher:
Release Date : 1982

An Engineering Method For Estimating The Aerodynamic Characteristics Of Circulation Control Wings Ccw written by Campbell Henderson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Jet flaps (Airplanes). categories.

Nasa Sp

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Author :
language : en
Publisher:
Release Date : 1993

Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.

Agard Index Of Publications

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Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
language : en
Publisher:
Release Date : 1989

Agard Index Of Publications written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aeronautics categories.

Upwind Design Limits And Solutions For Very Large Turbines

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Author :
language : en
Publisher: EWEA
Release Date :

Upwind Design Limits And Solutions For Very Large Turbines written by and has been published by EWEA this book supported file pdf, txt, epub, kindle and other format this book has been release on with categories.

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 1975-09

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975-09 with Government publications categories.