Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings
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Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings
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Author : Murray Pittel
language : en
Publisher:
Release Date : 1956
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings written by Murray Pittel 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.
Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from a Mach number M of 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings
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Author : Murray Pittel
language : en
Publisher:
Release Date : 1950
Flight Tests At Supersonic Speeds To Determine The Effect Of Taper On The Zero Lift Drag Of Sweptback Low Aspect Ratio Wings written by Murray Pittel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerodynamics, Supersonic categories.
Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from Mach number 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.
Analysis And Comparison With Theory Of Flow Field Measurements Near A Lifting Rotor In The Langley Full Scale Tunnel
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Author : Harry H. Heyson
language : en
Publisher:
Release Date : 1956
Analysis And Comparison With Theory Of Flow Field Measurements Near A Lifting Rotor In The Langley Full Scale Tunnel written by Harry H. Heyson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Air flow categories.
Results of an investigation in the Langley full-scale tunnel of the induced flow near a lifting rotor are given. Measurements of stream angles and velocities were made in several transverse planes along and behind the rotor in four different conditions representative of the cruising and high-speed ranges of flight. These measurements indicate that available theory may be used to calculate with reasonable accuracy the induced flow over the forward three-quarters of the disk for these flight conditions provided that a realistic nonuniform rotor disk-load distribution is assumed. Rearward of the three-quarter-diameter point, calculations of the induced velocity are increasingly inaccurate due to the rolling up of the trailing-vortex system. Farther rearward, well behind the rotor, the flow may be represented more accurately by the flow behind a uniformly loaded wing.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956
Technical Note 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 1956 with Aeronautics categories.
Flight Tests To Determine The Effect Of Taper On The Zero Lift Drag Of Wings At Low Supersonic Speeds
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Author : Sidney R. Alexander
language : en
Publisher:
Release Date : 1947
Flight Tests To Determine The Effect Of Taper On The Zero Lift Drag Of Wings At Low Supersonic Speeds written by Sidney R. Alexander and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aerodynamics, Supersonic categories.
Tests were conducted on wings having taper ratios from 0 to 1 mounted on rocket propelled test bodies to determine the effect of taper on the zero lift drag of wings at low supersonic speeds. Detailed data on models and test conditions are provided. comparison is made between results of theoretical drag calculations of tapered wings and applicable experimental values derived. Maximum thickness, leading edge, and trailing edge sweep are used in determining drag coefficient. At a constant leading edge sweep of 45 degree, no orderly variation of drag coefficient with taper ratio occurs.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1959
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 1959 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1954
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 1954 with Aeronautics categories.
Naca University Conference On Aerodynamics Construction And Propulsion
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Naca University Conference On Aerodynamics Construction And Propulsion 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 Aerodynamics categories.
Research Abstracts
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :
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 with Aeronautics categories.
Research Abstracts And Reclassification Notice
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Research Abstracts And Reclassification Notice 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.