A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Body Combination Designed For High Performance
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A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance
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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1961
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance written by Donald L. Loving 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.
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Body Combination Designed For High Performance
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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1956
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degrees Sweptback Wing Body Combination Designed For High Performance written by Donald L. Loving and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with categories.
Index Aeronauticus
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Author :
language : en
Publisher:
Release Date : 1962
Index Aeronauticus 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 Aeronautics categories.
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance
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Author : DONALD L. LOVING
language : en
Publisher:
Release Date : 1961
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Degree Sweptback Wing Body Combination Designed For High Performance written by DONALD L. LOVING 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.
The wing, designed to have high performance characteristics when used with an indented body, was tested in combination with an unindented body and bodies indented for mach numbers of 1.0, 1.2, an 1.4. At a given supersonic mach number, lowest values of zero-lift wave drag and highest values of maximum lift-drag ratio for the wingbody combinations were obtained at or near the specific mach number for which the body indentations were designed. Maximum lift-drag ratios of the order of 20 at subsonic speeds, 15 at mach number 1, 13 at mach 1.2, and 9 at mach 1.43 were obtained. Theoretically computed zero-lift wave drag was considered to be in good agreement with the experimental results.
Publications Announcements
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1958
Publications Announcements 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 1958 with Aeronautics categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1961
International Aerospace Abstracts 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 Aeronautics categories.
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Sweptback Wing Body Combination Designed For High Performance
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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1961
A Transonic Investigation Of Changing Indentation Design Mach Number On The Aerodynamic Characteristics Of A 45 Sweptback Wing Body Combination Designed For High Performance written by Donald L. Loving 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.
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.
An Experimental Transonic Investigation Of A 45 Sweptback Wing Body Combination With Several Types Of Body Indentation With Theoretical Comparisons Included
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Author : Melvin M. Carmel
language : en
Publisher:
Release Date : 1954
An Experimental Transonic Investigation Of A 45 Sweptback Wing Body Combination With Several Types Of Body Indentation With Theoretical Comparisons Included written by Melvin M. Carmel 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, Transonic categories.
Transonic Aerodynamic Characteristics Of A Wing Body Combination Having A 52 5 Deg Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of The Square Root 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 5 Deg Sweptback Wing Of Aspect Ratio 3 With Conical Camber And Designed For A Mach Number Of The Square Root 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 categories.