Transonic Aerodynamic Characteristics Of A Supersonic Transport Model With Variable Sweep Auxiliary Wing Panels Outboard Tail Surfaces And A Design Mach Number Of 2 6

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Transonic Aerodynamic Characteristics Of A Supersonic Cruise Aircraft Research Model With The Engines Suspended Above The Wing

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Author : Charles E. Mercer
language : en
Publisher:
Release Date : 1979

Transonic Aerodynamic Characteristics Of A Supersonic Cruise Aircraft Research Model With The Engines Suspended Above The Wing written by Charles E. Mercer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with categories.

Transonic Aerodynamic Characteristics Of A Supersonic Transport Model With Variable Sweep Auxiliary Wing Panels Outboard Tail Surfaces And A Design Mach Number Of 2 6

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Author : Roy V. Jr Harris
language : en
Publisher:
Release Date : 1965

Transonic Aerodynamic Characteristics Of A Supersonic Transport Model With Variable Sweep Auxiliary Wing Panels Outboard Tail Surfaces And A Design Mach Number Of 2 6 written by Roy V. Jr Harris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.

Transonic Aerodynamic Characteristics Of Supersonic Transport Model With A Fixed Warped Wing Having 74 Deg Sweep

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Author :
language : en
Publisher:
Release Date : 1965

Transonic Aerodynamic Characteristics Of Supersonic Transport Model With A Fixed Warped Wing Having 74 Deg Sweep written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.

Aerodynamic Characteristics Of A Three Engine Supersonic Transport Model Having A Low Aspect Ratio Variable Sweep Warped Wing

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Author : Odell A. Morris
language : en
Publisher:
Release Date : 1964

Aerodynamic Characteristics Of A Three Engine Supersonic Transport Model Having A Low Aspect Ratio Variable Sweep Warped Wing written by Odell A. Morris and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Airplanes categories.

Aerodynamic Characteristics Of A Tailless Fixed Wing Supersonic Transport Configuration At Mach Number 2 20

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Author : Gerald V. Foster
language : en
Publisher:
Release Date : 1964

Aerodynamic Characteristics Of A Tailless Fixed Wing Supersonic Transport Configuration At Mach Number 2 20 written by Gerald V. Foster and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Airplanes, Tailless categories.

Aerodynamic Characteristics At Mach 2 30 2 60 And 2 96 Of A Supersonic Transport Model With A Modified Wing

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Author :
language : en
Publisher:
Release Date : 1965

Aerodynamic Characteristics At Mach 2 30 2 60 And 2 96 Of A Supersonic Transport Model With A Modified Wing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.

Transonic Aerodynamics Characteristics Of A Supersonic Cruise Aircraft Research Model With The Engines Suspended Above The Wing

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Author : Charles E. Mercer
language : en
Publisher:
Release Date : 1979

Transonic Aerodynamics Characteristics Of A Supersonic Cruise Aircraft Research Model With The Engines Suspended Above The Wing written by Charles E. Mercer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aerodynamics, Transonic categories.

An investigation was conducted in the Langley ]6-foot transonic tunnel to determine the influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a supersonic cruise aircraft research configuration over a range of Mach numbers from 0.60 to 1.20. The arrow-wing transport configuration with engines suspended over the wing was tested at angles of attack from -4 ° to 6° and jet total-pressure ratios from ] to approximately 13. Wing-tip leading edge flap deflections of -10 ° to ]0 ° were tested with the wing-body configuration. Various nacelle locations (chordwise, spanwise, and vertical) were tested over the ranges of Mach numbers, angles of attack, and jet total-pressure ratios.

Nasa Technical Memorandum

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Author :
language : en
Publisher:
Release Date : 1979

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.

Aerodynamic Characteristics At Mach Numbers 2 30 2 60 And 2 96 Of A Supersonic Transport Model Having A Fixed Warped Wing

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Author :
language : en
Publisher:
Release Date : 1965

Aerodynamic Characteristics At Mach Numbers 2 30 2 60 And 2 96 Of A Supersonic Transport Model Having A Fixed Warped Wing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with categories.

Aerodynamic Characteristics Of A Three Engine Supersonic Transport Model Having A Low Aspect Ratio Variable Sweep Warped Wing

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Author :
language : en
Publisher:
Release Date : 1964

Aerodynamic Characteristics Of A Three Engine Supersonic Transport Model Having A Low Aspect Ratio Variable Sweep Warped Wing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.