Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 2 Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of 2

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Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 20 Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of 2

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Author : William B. Igoe
language : en
Publisher:
Release Date : 1961

Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 20 Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of 2 written by William B. Igoe and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aerodynamics categories.

Transonic Aerodynamic Loading Characteristics Of A Wing Body Tail Combination Having 52 5 Sweptback Wing Of Aspect Ratio 3 With Conical Wing Camber And Body Indentation For A Design Mach Number Square Root Of 2

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Author : Marlowe D. Cassetti
language : en
Publisher:
Release Date : 1961

Transonic Aerodynamic Loading Characteristics Of A Wing Body Tail Combination Having 52 5 Sweptback Wing Of Aspect Ratio 3 With Conical Wing Camber And Body Indentation For A Design Mach Number Square Root Of 2 written by Marlowe D. Cassetti and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Transonic wind tunnels categories.

An investigation has been made of the effects of conical wing camber and body indentation according to the supersonic area rule on the aerodynamic wing loading characteristics of a wing-body-tail configuration at transonic speeds. The wing aspect ratio was 3, taper ratio was 0.1, and quarter-chord-line sweepback was 52.5° with 3-percent-thick airfoil sections. The tests were conducted in the Langley 16-foot transonic tunnel at Mach numbers from 0.80 to 1.05 and at angles of attack from 0° to 14°, with Reynolds numbers based on mean aerodynamic chord varying from 7 x 106 to 8 x 106. Conical camber delayed wing-tip stall and reduced the severity of the accompanying longitudinal instability but did not appreciably affect the spanwise load distribution at angles of attack below tip stall. Body indentation reduced to transonic chordwise center-of-pressure travel from about 8 percent to 5 percent of the mean aerodynamic chord.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1961

Nasa Technical Note written by 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.

Index To Nasa Technical Publications

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07

Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with 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 : 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.

Monthly Catalog Of United States Government Publications Cumulative Index

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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1979

Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with United States categories.

Monthly Catalog Of United States Government Publications

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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1961

Monthly Catalog Of United States Government Publications written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Government publications categories.

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 1961

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Government publications categories.

Research Abstracts And Reclassification Notice

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956

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 1956 with Aeronautics categories.