Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Subsonic Canard Airplane Model Having A Wing With An Aspect Ratio Of 3 6 At Mach Numbers From 0 30 To 0 98
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Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Subsonic Canard Airplane Model Having A Wing With An Aspect Ratio Of 3 6 At Mach Numbers From 0 30 To 0 98
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Author :
language : en
Publisher:
Release Date : 1962
Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Subsonic Canard Airplane Model Having A Wing With An Aspect Ratio Of 3 6 At Mach Numbers From 0 30 To 0 98 written by 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.
Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1963
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Science categories.
Catalogues And Indexes Of British Government Publications 1920 1970 Annual Catalogues Of British Government Publications 1961 1970
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Author : Great Britain. Stationery Office
language : en
Publisher:
Release Date : 1974
Catalogues And Indexes Of British Government Publications 1920 1970 Annual Catalogues Of British Government Publications 1961 1970 written by Great Britain. Stationery Office and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Government publications categories.
Subsonic Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Canard Airplane Model Having A Wing With An Aspect Ratio Of 6 0
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Author :
language : en
Publisher:
Release Date : 1962
Subsonic Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Canard Airplane Model Having A Wing With An Aspect Ratio Of 6 0 written by 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.
Aerodynamic Characteristics Of A Canard And An Outboard Tail Airplane Model At High Subsonic Speeds
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Author : Paul G. Fournier
language : en
Publisher:
Release Date : 1961
Aerodynamic Characteristics Of A Canard And An Outboard Tail Airplane Model At High Subsonic Speeds written by Paul G. Fournier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamic load categories.
Longitudinal Aerodynamic Characteristics Of A High Subsonic Speed Transport Airplane Model With A Cambered 40 Deg Sweptback Wing Of Aspect Ratio 8 At Mach Numbers To 0 96
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Author :
language : en
Publisher:
Release Date : 1960
Longitudinal Aerodynamic Characteristics Of A High Subsonic Speed Transport Airplane Model With A Cambered 40 Deg Sweptback Wing Of Aspect Ratio 8 At Mach Numbers To 0 96 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Longitudinal Aerodynamic Characteristics Of A High Subsonic Speed Transport Airplane Model With A Cambered 40 Sweptback Wing Of Aspect Ratio 8 At Mach Numbers To 0 96
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Author : Atwood R. Heath
language : en
Publisher:
Release Date : 1960
Longitudinal Aerodynamic Characteristics Of A High Subsonic Speed Transport Airplane Model With A Cambered 40 Sweptback Wing Of Aspect Ratio 8 At Mach Numbers To 0 96 written by Atwood R. Heath and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Mach number categories.
Aerodynamic Characteristics Of A Canard And An Outboard Tail Airplane Model At High Subsonic Speeds
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Author : Paul G. Fournier
language : en
Publisher:
Release Date : 1961
Aerodynamic Characteristics Of A Canard And An Outboard Tail Airplane Model At High Subsonic Speeds written by Paul G. Fournier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
An investigation was made in the Langley highspeed 7- by 10-foot tunnel through a range of Mach numbers from 0.60 to 0.95 of the static longitudinal and lateral stability and control characteristics of a canard airplane configuration and an outboard-tail configuration. The canard model had a twisted wing with approximately 67 degrees o sweepback and an aspect ratio of 2.91 and was tested with three trapezoidal canard surfaces having ratios of exposed area to wing area of 0.032, 0.076, and 0.121. The canard model had a single body-mounted vertical tail. The outboard-tail model had its horizontal- and vertical-tail surfaces mounted on slender bodies attached to the wing tips and located to the rear and outboard of the 67 degrees sweptback wing of aspect ratio 1.00. The data, which are presented with limited analysis, provide information at high subsonic speeds on these two types of high-speed airplanes which have previously been tested at supersonic speeds and reported in NACA RM L58B07 and NACA RM L58E20 (AD-153 929 and AD-221 852). (Author).
Static Longitudinal Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 0 80 Chord Line Unswept And With Several Tail Configurations
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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1961
Static Longitudinal Characteristics At High Subsonic Speeds Of A Complete Airplane Model With A Highly Tapered Wing Having The 0 80 Chord Line Unswept And With Several Tail Configurations written by Kenneth W. Goodson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Stability of airplanes, Longitudinal categories.
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.
The Subsonic Static Aerodynamic Characteristics Of An Airplane Model Having A Triangular Wing Of Aspect Ratio 3
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Author : Howard F. Savage
language : en
Publisher:
Release Date : 1957
The Subsonic Static Aerodynamic Characteristics Of An Airplane Model Having A Triangular Wing Of Aspect Ratio 3 written by Howard F. Savage and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamics categories.
An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.