A Correlation Between Flight Determined Derivatives And Wind Tunnel Data For The X 24b Research Aircraft
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A Correlation Between Flight Determined Derivatives And Wind Tunnel Data For The X 24b Research Aircraft
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Author :
language : en
Publisher:
Release Date : 1997
A Correlation Between Flight Determined Derivatives And Wind Tunnel Data For The X 24b Research Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with categories.
Nasa Technical Paper
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Author :
language : en
Publisher:
Release Date : 1980
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Science categories.
Nasa Reference Publication
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Author :
language : en
Publisher:
Release Date : 1977
Nasa Reference Publication written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Astronautics categories.
Development Of The X 33 Aerodynamic Uncertainty Model
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Author : Brent R. Cobleigh
language : en
Publisher:
Release Date : 1998
Development Of The X 33 Aerodynamic Uncertainty Model written by Brent R. Cobleigh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics categories.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1986
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 1986 with Aeronautics categories.
From Runway To Orbit
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Author : Kenneth W. Iliff
language : en
Publisher: History Office
Release Date : 2004
From Runway To Orbit written by Kenneth W. Iliff and has been published by History Office this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004 with Biography & Autobiography categories.
NOTE: NO FURTHER DISCOUNT FOR THIS PRINT PRODUCT--OVERSTOCK SALE -- Significantly reduced list price while supplies last NASA SP 2004-4109. NASA History Series. Presents the memoirs of Dr. Kenneth W. Iliff, the retired Chief Scientist of NASA Dryden Flight Research Center. He worked at NASA from 1962-2002. Related products: Commercial Orbital Transportation Services: A New Era in Spaceflight is available here: https: //bookstore.gpo.gov/products/sku/033-000-01367-1 Reference Guide to the International Space Station is available here: https: //bookstore.gpo.gov/products/sku/033-000-01373-6 Other products produced by the U.S. National Aeronautics and Space Administration (NASA) can be found here: https: //bookstore.gpo.gov/agency/550"
Aerodynamic Derivative Characteristics Of The X 15 Research Airplane As Determined From Flight Tests For Mach Numbers From 0 6 To 3 4
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Author : Roxanah B. Yancey
language : en
Publisher:
Release Date : 1962
Aerodynamic Derivative Characteristics Of The X 15 Research Airplane As Determined From Flight Tests For Mach Numbers From 0 6 To 3 4 written by Roxanah B. Yancey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with categories.
Comparison Of Flight Test And Wind Tunnel Performance Characteristics Of The X 24b Research Aircraft
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Author : David F. Richardson
language : en
Publisher:
Release Date : 1976
Comparison Of Flight Test And Wind Tunnel Performance Characteristics Of The X 24b Research Aircraft written by David F. Richardson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
This report presents the flight-determined lift and drag characteristics of the X-24B research aircraft and compares them to wind tunnel predictions. Lift and drag data were computed from onboard measured accelerations and flight conditions while the aircraft was in gliding flight. Performance data were obtained up to a maximum Mach number of 1.72. Flight test and wind tunnel data were in general agreement, although the lift curve slope was less than predicted at most Mach numbers. The drag-due-to-lift was higher than predicted in all cases. Values of maximum lift-to-drag ratio were less than predicted for all flight conditions where comparisons could be made. The maximum subsonic lift-to-drag ratio was 4.5. (Author).
Aerodynamic Assessment Of Flight Determined Subsonic Lift And Drag Characteristics Of Seven Lifting Body And Wing Body Reentry Vehicle Configurations
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Author : Edwin J. Saltzman
language : en
Publisher:
Release Date : 2002
Aerodynamic Assessment Of Flight Determined Subsonic Lift And Drag Characteristics Of Seven Lifting Body And Wing Body Reentry Vehicle Configurations written by Edwin J. Saltzman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Drag (Aerodynamics) categories.
Stability And Control Of Conventional And Unconventional Aerospace Vehicle Configurations
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Author : Bernd Chudoba
language : en
Publisher: Springer
Release Date : 2019-07-23
Stability And Control Of Conventional And Unconventional Aerospace Vehicle Configurations written by Bernd Chudoba and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2019-07-23 with Technology & Engineering categories.
This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
