Effect Of Horizontal Tail Size And Tail Length On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces
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Effect Of Horizontal Tail Size And Tail Length On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces
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Author : Jacob H. Lichtenstein
language : en
Publisher:
Release Date : 1951
Effect Of Horizontal Tail Size And Tail Length On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces written by Jacob H. Lichtenstein and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Airplanes categories.
Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.
Experimental Determination Of The Effect Of Horizontal Tail Size Tail Length And Vertical Location On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces
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Author : Arthur Earl Bryson
language : en
Publisher:
Release Date : 1952
Experimental Determination Of The Effect Of Horizontal Tail Size Tail Length And Vertical Location On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces written by Arthur Earl Bryson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aeronautics categories.
Research Abstracts
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951
Research Abstracts written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aeronautics categories.
Theoretical Study Of The Tunnel Boundary Lift Interference Due To Slotted Walls In The Presence Of The Trailing Vortex System Of A Lifting Model
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Author : Clarence W. Matthews
language : en
Publisher:
Release Date : 1955
Theoretical Study Of The Tunnel Boundary Lift Interference Due To Slotted Walls In The Presence Of The Trailing Vortex System Of A Lifting Model written by Clarence W. Matthews and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Report
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Author :
language : en
Publisher:
Release Date : 1955
Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aeronautics categories.
Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.
Annual Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957
Annual Report National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1949
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.
Rectangular Wind Tunnel Blocking Corrections Using The Velocity Ratio Method
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Author : Rudolph W. Hensel
language : en
Publisher:
Release Date : 1951
Rectangular Wind Tunnel Blocking Corrections Using The Velocity Ratio Method written by Rudolph W. Hensel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Mathematical analysis categories.
Calculations of the ratios of the velocity increments at test bodies to those at the tunnel walls caused by the solid blocking of these bodies within the walls of a closed rectangular wind tunnel are presented. The boides treated include two-dimensional airfoils; small bodies of revolution; straight, untapered, finite-span wings of varying span; and swept, untapered, finite-span wings of varying span. It is shown that, after wake blocking effects have been removed , the present method furnishes semiempirical blocking corrections for most wind-tunnel models and their components. The test section proportions of the Southern California Cooperative Wind Tunnel at CIT (ratio of height to width equal to 1/square root of 2) are used in the calculations.