Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
A Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft
Author: NASA Technical Paper
Author: NASA Reference Publication
Author: Development of the X-33 Aerodynamic Uncertainty Model
Author: Brent R. CobleighPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40
Book Description
NASA Technical Memorandum
Author: From Runway to Orbit
Author: Kenneth W. IliffPublisher: History Office
ISBN:
Category : Biography & Autobiography
Languages : en
Pages : 432
Book Description
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
Author: Edwin J. SaltzmanPublisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 162
Book Description
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations
Author: Bernd ChudobaPublisher: Springer
ISBN: 3030168565
Category : Technology & Engineering
Languages : en
Pages : 392
Book Description
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
Author: Roxanah B. YanceyThe Theory and Practice of Estimating the Accuracy of Dynamic Flight-determined Coefficients
Author: Richard E. MainePublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 72
Book Description