Author: Dave Windle
Publisher: Casemate Publishers
ISBN: 1848844085
Category : Transportation
Languages : en
Pages : 71
Book Description
The Vought F4U was the best carrier based fighter of WW2. 12,571 aircraft were built and downed 2,140 enemy aircraft for the loss of only 189 Corsairs. It was developed early in 1938 for the US Navy. The designer, Tex Beisel, worked on the principle of the largest engine in the smallest airframe. Britain received 2012 of the type. This book contains the world famous color profiles created by Dave Windle of the type in different operational modes, configurations and color schemes. Martin Bowman has written detailed descriptions and photographs to create the perfect enthusiasts reference.
Profiles of Flight
Author: Dave Windle
Publisher: Casemate Publishers
ISBN: 1848844085
Category : Transportation
Languages : en
Pages : 71
Book Description
The Vought F4U was the best carrier based fighter of WW2. 12,571 aircraft were built and downed 2,140 enemy aircraft for the loss of only 189 Corsairs. It was developed early in 1938 for the US Navy. The designer, Tex Beisel, worked on the principle of the largest engine in the smallest airframe. Britain received 2012 of the type. This book contains the world famous color profiles created by Dave Windle of the type in different operational modes, configurations and color schemes. Martin Bowman has written detailed descriptions and photographs to create the perfect enthusiasts reference.
Publisher: Casemate Publishers
ISBN: 1848844085
Category : Transportation
Languages : en
Pages : 71
Book Description
The Vought F4U was the best carrier based fighter of WW2. 12,571 aircraft were built and downed 2,140 enemy aircraft for the loss of only 189 Corsairs. It was developed early in 1938 for the US Navy. The designer, Tex Beisel, worked on the principle of the largest engine in the smallest airframe. Britain received 2012 of the type. This book contains the world famous color profiles created by Dave Windle of the type in different operational modes, configurations and color schemes. Martin Bowman has written detailed descriptions and photographs to create the perfect enthusiasts reference.
Gust Loads on Aircraft
Author: Frederic M. Hoblit
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
Microwave Refractive Index Structure Function Profiles (CN2) Measured from a Small Aircraft
Author: James F. Morrissey
Publisher:
ISBN:
Category : Atmospheric radio refractivity
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Atmospheric radio refractivity
Languages : en
Pages : 36
Book Description
EPA-600/4
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Profiles of Flight
Author: Dave Windle
Publisher: Casemate Publishers
ISBN: 9781848842373
Category : History
Languages : en
Pages : 0
Book Description
This versatile single-seater aircraft was a joint development between the UK and France. It first flew in 1968, but its robust and flexible operational uses led to its long service life, only being retired from RAF service in 2008. It has seen front-line action in all major conflicts since introduced and has been exported to India, Ecuador, Nigeria and Oman.This book contains the world famous color profiles created by Dave Windle of the type in different operational modes, con
Publisher: Casemate Publishers
ISBN: 9781848842373
Category : History
Languages : en
Pages : 0
Book Description
This versatile single-seater aircraft was a joint development between the UK and France. It first flew in 1968, but its robust and flexible operational uses led to its long service life, only being retired from RAF service in 2008. It has seen front-line action in all major conflicts since introduced and has been exported to India, Ecuador, Nigeria and Oman.This book contains the world famous color profiles created by Dave Windle of the type in different operational modes, con
Military Standard
Author: United States. Department of Defense
Publisher:
ISBN:
Category : Environmental engineering
Languages : en
Pages : 456
Book Description
Publisher:
ISBN:
Category : Environmental engineering
Languages : en
Pages : 456
Book Description
Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021)
Author: Meiping Wu
Publisher: Springer Nature
ISBN: 9811694923
Category : Technology & Engineering
Languages : en
Pages : 3575
Book Description
This book includes original, peer-reviewed research papers from the ICAUS 2021, which offers a unique and interesting platform for scientists, engineers and practitioners throughout the world to present and share their most recent research and innovative ideas. The aim of the ICAUS 2021 is to stimulate researchers active in the areas pertinent to intelligent unmanned systems. The topics covered include but are not limited to Unmanned Aerial/Ground/Surface/Underwater Systems, Robotic, Autonomous Control/Navigation and Positioning/ Architecture, Energy and Task Planning and Effectiveness Evaluation Technologies, Artificial Intelligence Algorithm/Bionic Technology and Its Application in Unmanned Systems. The papers showcased here share the latest findings on Unmanned Systems, Robotics, Automation, Intelligent Systems, Control Systems, Integrated Networks, Modeling and Simulation. It makes the book a valuable asset for researchers, engineers, and university students alike.
Publisher: Springer Nature
ISBN: 9811694923
Category : Technology & Engineering
Languages : en
Pages : 3575
Book Description
This book includes original, peer-reviewed research papers from the ICAUS 2021, which offers a unique and interesting platform for scientists, engineers and practitioners throughout the world to present and share their most recent research and innovative ideas. The aim of the ICAUS 2021 is to stimulate researchers active in the areas pertinent to intelligent unmanned systems. The topics covered include but are not limited to Unmanned Aerial/Ground/Surface/Underwater Systems, Robotic, Autonomous Control/Navigation and Positioning/ Architecture, Energy and Task Planning and Effectiveness Evaluation Technologies, Artificial Intelligence Algorithm/Bionic Technology and Its Application in Unmanned Systems. The papers showcased here share the latest findings on Unmanned Systems, Robotics, Automation, Intelligent Systems, Control Systems, Integrated Networks, Modeling and Simulation. It makes the book a valuable asset for researchers, engineers, and university students alike.
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 170
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 170
Book Description
Battle of Britain Memorial Flight in Profile
Author: Chris Sandham-Bailey
Publisher:
ISBN: 9781911658450
Category :
Languages : en
Pages :
Book Description
The Battle of Britain Memorial Flight (BBMF) is a standing reminder of the heroism and sacrifice of countless British and Commonwealth aircrew who flew and fought during the Second World War.Formed at RAF Biggin Hill on July 11, 1957, as the Historic Aircraft Flight, today the BBMF's incredible collection of aircraft includes six Spitfires, two Hurricanes, one of only two airworthy Avro Lancaster bombers in the world, a Douglas C-47 Dakota and two de Havilland Chipmunks.The Flight's Second World War aircraft have survived against the odds to exist in flying condition today and this book charts each of their careers over the last seven decades or more.Author and illustrator Chris Sandham-Bailey has meticulously reproduced every known paint scheme worn by each of the aircraft - as well as gathering together an unrivaled collection of photographs to show how the appearance of the aircraft has changed.Never before have all of the BBMF aircraft liveries from the war's end to the present day been catalogued and illustrated in one publication. This book is a must for anyone with an interest in the BBMF aircraft and their histories.
Publisher:
ISBN: 9781911658450
Category :
Languages : en
Pages :
Book Description
The Battle of Britain Memorial Flight (BBMF) is a standing reminder of the heroism and sacrifice of countless British and Commonwealth aircrew who flew and fought during the Second World War.Formed at RAF Biggin Hill on July 11, 1957, as the Historic Aircraft Flight, today the BBMF's incredible collection of aircraft includes six Spitfires, two Hurricanes, one of only two airworthy Avro Lancaster bombers in the world, a Douglas C-47 Dakota and two de Havilland Chipmunks.The Flight's Second World War aircraft have survived against the odds to exist in flying condition today and this book charts each of their careers over the last seven decades or more.Author and illustrator Chris Sandham-Bailey has meticulously reproduced every known paint scheme worn by each of the aircraft - as well as gathering together an unrivaled collection of photographs to show how the appearance of the aircraft has changed.Never before have all of the BBMF aircraft liveries from the war's end to the present day been catalogued and illustrated in one publication. This book is a must for anyone with an interest in the BBMF aircraft and their histories.
Flight Investigation of Boundary-layer and Profile-drag Characteristics of Smooth Wing Sections of a P-47D Airplane
Author: John A. Zalovcik
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Summary: A flight investigation was made of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane. Measurements were made at three stations on the wing: boundary-layer measurements were made on the upper surface of the left wing in the slip-stream at 25 percent semispan; pressure-distribution measurements were made on the upper surface of the left wing at 63 percent semispan; and wake surveys were made at 63 percent semispan of the right wing. The tests were made in straight flight and in turns over a range of conditions in which airplane lift coefficients from 0.15 to 0.68, Reynolds numbers from 7.7 x 106 to 19.7 x 106, and Mach numbers from 0.25 to 0.69 were obtained. The results of the investigation indicated a minimum profile-drag coefficient of 0.0062 for the smooth section at 63 percent semispan. At the highest Mach number attained in the tests, the critical Mach number was exceeded by at least 0.04 with no evidence of compressibility shock losses appearing in the form of increased width of the wake or increased profile-drag coefficient. For flight conditions approaching the critical Mach number, variations in Mach number of as much as 0.17 appeared to have no effect on the profile-drag coefficient. In the slipstream, transition occurred at least as far back as 20 percent chord on the upper surface at low lift coefficients.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Summary: A flight investigation was made of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane. Measurements were made at three stations on the wing: boundary-layer measurements were made on the upper surface of the left wing in the slip-stream at 25 percent semispan; pressure-distribution measurements were made on the upper surface of the left wing at 63 percent semispan; and wake surveys were made at 63 percent semispan of the right wing. The tests were made in straight flight and in turns over a range of conditions in which airplane lift coefficients from 0.15 to 0.68, Reynolds numbers from 7.7 x 106 to 19.7 x 106, and Mach numbers from 0.25 to 0.69 were obtained. The results of the investigation indicated a minimum profile-drag coefficient of 0.0062 for the smooth section at 63 percent semispan. At the highest Mach number attained in the tests, the critical Mach number was exceeded by at least 0.04 with no evidence of compressibility shock losses appearing in the form of increased width of the wake or increased profile-drag coefficient. For flight conditions approaching the critical Mach number, variations in Mach number of as much as 0.17 appeared to have no effect on the profile-drag coefficient. In the slipstream, transition occurred at least as far back as 20 percent chord on the upper surface at low lift coefficients.