A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback
DOWNLOAD
Download A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback
DOWNLOAD
Author : Jack D. Stephenson
language : en
Publisher:
Release Date : 1955
A Comparison At Mach Numbers Up To 0 92 Of The Calculated And Experimental Downwash And Wake Characteristics At Various Horizonatl Tail Heights Behind A Wing With 45 Degrees Of Sweepback written by Jack D. Stephenson 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.
Comparison Between Experimental And Predicted Downwash At A Mach Number Of 0 25 Behind A Wing Body Combination Having A Triangular Wing Of Aspect Ratio 2 0
DOWNLOAD
Author : Norman E. Sorenson
language : en
Publisher:
Release Date : 1956
Comparison Between Experimental And Predicted Downwash At A Mach Number Of 0 25 Behind A Wing Body Combination Having A Triangular Wing Of Aspect Ratio 2 0 written by Norman E. Sorenson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.
A study was undertaken to evaluate a method for predicting the downwash in a transverse plane behind a wing-body combination throughout an angle-of-attack range from 0 to 20 degrees. The predicted downwash was calculated by a numerical method in which an array of discrete vortices was allowed to roll up. The wing vortices were assumed to emanate from the trailing edge of the wing with their positions and strengths determined from the measured spanwise distribution of load.
Effectiveness Of An All Movable Horizontal Tail On An Unswept Wing And Body Combination For Mach Numbers From 0 60 To 1 40
DOWNLOAD
Author : Louis S. Stivers
language : en
Publisher:
Release Date : 1959
Effectiveness Of An All Movable Horizontal Tail On An Unswept Wing And Body Combination For Mach Numbers From 0 60 To 1 40 written by Louis S. Stivers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Mach number categories.
The Effective Downwash Characteristics At Transonic Speeds Of A 6 Percent Thick Wing With 47 Degrees Of Sweepback In Combination With A Cylindrical Body As Determined From Force Measurements Of A Horizontal Tail
DOWNLOAD
Author : Domenic A. Coppolino
language : en
Publisher:
Release Date : 1952
The Effective Downwash Characteristics At Transonic Speeds Of A 6 Percent Thick Wing With 47 Degrees Of Sweepback In Combination With A Cylindrical Body As Determined From Force Measurements Of A Horizontal Tail written by Domenic A. Coppolino and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Downwash Characteristics And Vortex Sheet Shape Behind A 63 Degree Swept Back Wing Fuselage Combination At A Reynolds Number Of 6 100 000
DOWNLOAD
Author : William H. Tolhurst (Jr.)
language : en
Publisher:
Release Date : 1952
Downwash Characteristics And Vortex Sheet Shape Behind A 63 Degree Swept Back Wing Fuselage Combination At A Reynolds Number Of 6 100 000 written by William H. Tolhurst (Jr.) 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.
It was found that at positie angles of attack the vortex sheet assumed a shape which was initially bowed upward but flattened out downstream before the rolling-up process had progressed to an appreciable degree. A comparison with theory showed that an acceptable approximation tothe downwash distribution within the distance surveyed could be obtained if the vortex sheet were assumed to be flat and the spanwise vorticity distribution were assumed to be that of the wing.
Investigation Of The Downwash And Wake Behind A Triangular Wing Of Aspect Ratio 4 At Subsonic And Supersonic Mach Numbers
DOWNLOAD
Author : Harold J. Walker
language : en
Publisher:
Release Date : 1950
Investigation Of The Downwash And Wake Behind A Triangular Wing Of Aspect Ratio 4 At Subsonic And Supersonic Mach Numbers written by Harold J. Walker and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Airplanes categories.
The effects of Mach number in the ranges between 0.50 and 0.95 and between 1.09 and 1.29 on the characteristics of the downwash and on the location of the wake behind a triangular wing of aspect ratio 4 have been determined from semispan model tests.
An Analysis Of Estimated And Experimental Transonic Downwash Characteristics As Affected By Plan Form And Thickness For Wing And Wing Fuselage Configurations
DOWNLOAD
Author : Joseph Weil
language : en
Publisher:
Release Date : 1956
An Analysis Of Estimated And Experimental Transonic Downwash Characteristics As Affected By Plan Form And Thickness For Wing And Wing Fuselage Configurations written by Joseph Weil and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.
As part of a transonic research program the sensitivity of downwash at the tail plane to fairly systematic changes in wing plan form and thickness has been evaluated over a Mach number range of approximately 0.6 to 1.1, utilizing the transonic-bump technique. This paper presents a summary of information obtained from 11 transonic-bump investigations of wing and wing-fuselage configurations and compares the experimental results with theoretical estimations made for subsonic and supersonic Mach numbers.
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1971
Experimental Wake Survey Behind A 120 Deg Included Angle Cone At Angles Of Attack Of 0 Deg And 5 Deg Mach Numbers From 1 60 To 3 95 And Longitudinal Stations Varying From 1 0 To 8 39 Body Diameters written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with categories.
The Longitudinal Characteristics At Mach Numbers Up To 0 92 Of A Cambered And Twisted Wing Having 40 Degrees Of Sweepback And An Aspect Ratio Of 10
DOWNLOAD
Author : George G. Edwards
language : en
Publisher:
Release Date : 1952
The Longitudinal Characteristics At Mach Numbers Up To 0 92 Of A Cambered And Twisted Wing Having 40 Degrees Of Sweepback And An Aspect Ratio Of 10 written by George G. Edwards and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.
Downwash Sidewash And Wave Survey Behind A 420 Sweptback Wing At A Reynolds Number Of 6 8 X 106 With And Without A Simulated Ground
DOWNLOAD
Author : G. Chester Furlong
language : en
Publisher:
Release Date : 1948
Downwash Sidewash And Wave Survey Behind A 420 Sweptback Wing At A Reynolds Number Of 6 8 X 106 With And Without A Simulated Ground written by G. Chester Furlong and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aiprlanes categories.