A Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft by :

Download or read book A Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft written by and published by . This book was released on 1997 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Reference Publication

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ISBN 13 :
Total Pages : 532 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Reference Publication by :

Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Development of the X-33 Aerodynamic Uncertainty Model

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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Development of the X-33 Aerodynamic Uncertainty Model by : Brent R. Cobleigh

Download or read book Development of the X-33 Aerodynamic Uncertainty Model written by Brent R. Cobleigh and published by . This book was released on 1998 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (319 download)

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Download or read book NASA Technical Memorandum written by and published by . This book was released on 1986 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

From Runway to Orbit

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Publisher : History Office
ISBN 13 :
Total Pages : 432 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis From Runway to Orbit by : Kenneth W. Iliff

Download or read book From Runway to Orbit written by Kenneth W. Iliff and published by History Office. This book was released on 2004 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Assessment of Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations by : Edwin J. Saltzman

Download or read book 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 published by . This book was released on 2002 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations

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Publisher : Springer
ISBN 13 : 3030168565
Total Pages : 392 pages
Book Rating : 4.0/5 (31 download)

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Book Synopsis Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations by : Bernd Chudoba

Download or read book Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations written by Bernd Chudoba and published by Springer. This book was released on 2019-07-23 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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?

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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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4 by : Roxanah B. Yancey

Download or read book 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 published by . This book was released on 1962 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Theory and Practice of Estimating the Accuracy of Dynamic Flight-determined Coefficients

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ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis The Theory and Practice of Estimating the Accuracy of Dynamic Flight-determined Coefficients by : Richard E. Maine

Download or read book The Theory and Practice of Estimating the Accuracy of Dynamic Flight-determined Coefficients written by Richard E. Maine and published by . This book was released on 1981 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comparison of Flight Test and Wind Tunnel Performance Characteristics of the X-24B Research Aircraft

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Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Comparison of Flight Test and Wind Tunnel Performance Characteristics of the X-24B Research Aircraft by : David F. Richardson

Download or read book Comparison of Flight Test and Wind Tunnel Performance Characteristics of the X-24B Research Aircraft written by David F. Richardson and published by . This book was released on 1976 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Fifty Years of Flight Research

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ISBN 13 :
Total Pages : 526 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Fifty Years of Flight Research by : David F. Fisher

Download or read book Fifty Years of Flight Research written by David F. Fisher and published by . This book was released on 1999 with total page 526 pages. Available in PDF, EPUB and Kindle. Book excerpt: A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 684 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1979 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1998 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Selected Listing of NASA Scientific and Technical Reports for ...

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ISBN 13 :
Total Pages : 1680 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1965 with total page 1680 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Scientific and Technical Reports

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ISBN 13 :
Total Pages : 1440 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1966 with total page 1440 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane

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ISBN 13 :
Total Pages : 204 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane by : Ernest L. Black

Download or read book Correlation of Aerodynamic Stability and Control Derivatives Obtained from Flight Tests and Wind Tunnel Tests on the XC-142A Airplane written by Ernest L. Black and published by . This book was released on 1969 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt: