Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4

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Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4

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Author : Clarence L. Gillis
language : en
Publisher:
Release Date : 1959

Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 written by Clarence L. Gillis 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.

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 : 1957

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 1957 with Aeronautics categories.

The Journal Of The Royal Aeronautical Society

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Author :
language : en
Publisher:
Release Date : 1960

The Journal Of The Royal Aeronautical Society 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 Aeronautics categories.

Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4

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Author : Clarence L. Gillis
language : en
Publisher:
Release Date : 1959

Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 written by Clarence L. Gillis 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.

Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Tapered Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4

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Author : Clarence L. Gillis
language : en
Publisher:
Release Date : 1951

Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Tapered Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 written by Clarence L. Gillis and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with categories.

Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model

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Author : A. James Vitale
language : en
Publisher:
Release Date : 1952

Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model written by A. James Vitale 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.

Static Lateral 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 Configuration

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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1961

Static Lateral 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 Configuration 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, Lateral categories.

An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing had a taper of 0.067 and an unswept 0.80 chord line. The complete model was tested with a wing-chord-plane tail, a T-tail, and a biplane tail (combined T-tail and wing-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 over a range of angle of attack of about ±20° and a range of sideslip of -15° to 13°. Some data were obtained with the horizontal stabilizer deflected. A few tests were also made with the wing tips clipped to an aspect ratio of 3.00.

Aerodynamic Characteristics Of A 60 Degree Sweptback Wing Airplane Configuration Having Tail Surfaces Located Outboard Of The Wing Tips At Mach Numbers Of 2 30 2 97 3 51 And 4 06

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Author :
language : en
Publisher:
Release Date : 1960

Aerodynamic Characteristics Of A 60 Degree Sweptback Wing Airplane Configuration Having Tail Surfaces Located Outboard Of The Wing Tips At Mach Numbers Of 2 30 2 97 3 51 And 4 06 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.

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.