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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Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1965
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics 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.
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Having A 45 Degree Swept Wing Of Aspect Ratio 6 0
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Author : John C. McFall
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Having A 45 Degree Swept Wing Of Aspect Ratio 6 0 written by John C. McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamic load categories.
Longitudinal Stability And Control Characteristics At High Subsonic Speeds Of Two Models Of A Transonic Research Airplane With Wings And Horizontal Tails Of Aspect Ratios 4 2 And 2
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Author : Arvo A. Luoma
language : en
Publisher:
Release Date : 1950
Longitudinal Stability And Control Characteristics At High Subsonic Speeds Of Two Models Of A Transonic Research Airplane With Wings And Horizontal Tails Of Aspect Ratios 4 2 And 2 written by Arvo A. Luoma 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.
An investigation was made in the Langley 8-foot high-speed tunnel of two transonic research airplane models for Mach numbers up to approximately 0.95. The test Reynolds number at the highest speed was 1,600,000 for one model and 2,300,000 for the other model. The models were 1/16-schale and were supported in the tunnel on a sting. The wing and horizontal tail of one model were both of aspect ratio 4.2; the wing and horizontal tail of the other model were both of aspect ratio 2. The same fuselage and vertical tail were used on both models. The sweep of the 50-percent-chord line of the wings was zero degrees; the sweep of the 75-percent-chord line of the horizontal tails was zero degrees. Both wings had NACA 65-110 airfoil sections and both horizontal tails had NACA 65-008 airfoil sections. Lift drag, and pitching moment were determined by means of a strain-gage balance within the fuselage. Tare measurements were made to eliminate the interference effect of the sting.
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0
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Author : John C. Jr McFall
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Swept Wing Of Aspect Ratio 6 0 written by John C. Jr McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with categories.
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section 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 1954 with Airplanes categories.
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.
Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6
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Author : John D. Morrow
language : en
Publisher:
Release Date : 1953
Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6 written by John D. Morrow and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.
Stability And Drag Characteristics At Mach Numbers From 0 8 To 1 5 Of A Free Flight Model Having 3 Percent Thick 60 Degree Triangular Wing And Horizontal Tail Surfaces
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Author : Rowe Chapman
language : en
Publisher:
Release Date : 1954
Stability And Drag Characteristics At Mach Numbers From 0 8 To 1 5 Of A Free Flight Model Having 3 Percent Thick 60 Degree Triangular Wing And Horizontal Tail Surfaces written by Rowe Chapman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
A flight test of a rocket-propelled model having 60 degree triangular wing and horizontal tail surfaces 3 percent thick was made to investigate the stability and drag of the configuration. Drag and stability data are compared with similar triangular-wing configurations.
Lift Drag And Longitudinal Stability At Mach Numbers From 1 4 To 2 3 Of A Rocket Powered Model Having A 52 5 Degree Sweptback Wing Of Aspect Ratio 3 And Inline Tail Surfaces
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Author : Warren Jr Gillespie
language : en
Publisher:
Release Date : 1955
Lift Drag And Longitudinal Stability At Mach Numbers From 1 4 To 2 3 Of A Rocket Powered Model Having A 52 5 Degree Sweptback Wing Of Aspect Ratio 3 And Inline Tail Surfaces written by Warren Jr Gillespie and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with categories.
Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions
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Author : James H. Parks
language : en
Publisher:
Release Date : 1953
Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions written by James H. Parks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.