Author : Martin D. Maisel
Publisher : Unknown
Page : 222 pages
File Size : 53,9 Mb
Release : 2000
Category : Aeronautics
ISBN : UIUC:30112048584947
The History Of The Xv 15 Tilt Rotor Research Aircraft From Concept To Flight
The History Of The Xv 15 Tilt Rotor Research Aircraft From Concept To Flight Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of The History Of The Xv 15 Tilt Rotor Research Aircraft From Concept To Flight book. This book definitely worth reading, it is an incredibly well-written.
The History of the Xv-15 Tilt Rotor Research Aircraft from Concept to Flight
Author : Martin D. Maisel,Nasa Technical Reports Server (Ntrs),Et Al
Publisher : BiblioGov
Page : 224 pages
File Size : 44,6 Mb
Release : 2013-06
Category : Electronic
ISBN : 1289146373
The History of the Xv-15 Tilt Rotor Research Aircraft from Concept to Flight by Martin D. Maisel,Nasa Technical Reports Server (Ntrs),Et Al Pdf
This monograph is a testament to the efforts of many people overcoming multiple technical challenges encountered while developing the XV-15 tilt rotor research aircraft. The Ames involvement with the tilt rotor aircraft began in 1957 with investigations of the performance and dynamic behavior of the Bell XV-3 tilt rotor aircraft. At that time, Ames Research Center was known as the Ames Aeronautical Laboratory of the National Advisory Committee for Aeronautics (NACA). As we approach the new millennium, and after more than 40 years of effort and the successful completion of our initial goals, it is appropriate to reflect on the technical accomplishments and consider the future applications of this unique aircraft class, the tilt rotor. The talented engineers, technicians, managers, and leaders at Ames have worked hard with their counterparts in the U.S. rotorcraft industry to overcome technology barriers and to make the military and civil tilt rotor aircraft safer, environmentally acceptable, and more efficient. The tilt rotor aircraft combines the advantages of vertical takeoff and landing capabilities, inherent to the helicopter, with the forward speed and range of a fixed wing turboprop airplane. Our studies have shown that this new vehicle type can provide the aviation transportation industry with the flexibility for highspeed, long-range flight, coupled with runway-independent operations, thus having a significant potential to relieve airport congestion. We see the tilt rotor aircraft as an element of the solution to this growing air transport problem.
The History of the XV-15 Tilt Rotor Research Aircraft
Author : Martin D. Maisel,Demo J. Giulianetti,Daniel C. Dugan
Publisher : Government Reprints Press
Page : 0 pages
File Size : 42,8 Mb
Release : 2001-06
Category : Technology & Engineering
ISBN : 1931641277
The History of the XV-15 Tilt Rotor Research Aircraft by Martin D. Maisel,Demo J. Giulianetti,Daniel C. Dugan Pdf
Beskriver det amerikanske forsøgsprojekt med en Tilt Rotor på en flyvemaskine
The History of the XV-15 Tilt Rotor Research Aircraft: from Concept to Flight
Author : Martin Maisel,Demo Giulianetti,Daniel Dugan
Publisher : CreateSpace
Page : 220 pages
File Size : 55,7 Mb
Release : 2012-07-13
Category : Electronic
ISBN : 1478239573
The History of the XV-15 Tilt Rotor Research Aircraft: from Concept to Flight by Martin Maisel,Demo Giulianetti,Daniel Dugan Pdf
This monograph is a testament to the efforts of many people overcoming multiple technical challenges encountered while developing the XV-15 tilt rotor research aircraft.
The XV-15 Tilt Rotor Research Aircraft
Author : Anonim
Publisher : Unknown
Page : 50 pages
File Size : 55,9 Mb
Release : 1980
Category : Electronic
ISBN : NASA:31769000547581
The XV-15 Tilt Rotor Research Aircraft by Anonim Pdf
NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research
Author : Anonim
Publisher : Unknown
Page : 1064 pages
File Size : 41,6 Mb
Release : 2010
Category : Aeronautics
ISBN : UCSD:31822036341212
NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research by Anonim Pdf
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, *
Author : Anonim
Publisher : Unknown
Page : 1066 pages
File Size : 44,6 Mb
Release : 2011
Category : Electronic
ISBN : STANFORD:36105050567168
NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * by Anonim Pdf
NASA's Contributions to Aeronautics
Author : Anonim
Publisher : Unknown
Page : 980 pages
File Size : 49,6 Mb
Release : 2010
Category : Aeronautics
ISBN : IND:30000132750666
NASA's Contributions to Aeronautics by Anonim Pdf
NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls
Author : Anonim
Publisher : Unknown
Page : 980 pages
File Size : 51,7 Mb
Release : 2010
Category : Aeronautics
ISBN : UCSD:31822036341055
NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls by Anonim Pdf
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
Advances in Transitional Flow Modeling
Author : Chunhua Sheng
Publisher : Springer
Page : 130 pages
File Size : 44,7 Mb
Release : 2016-11-26
Category : Technology & Engineering
ISBN : 9783319325767
Advances in Transitional Flow Modeling by Chunhua Sheng Pdf
This book provides a comprehensive description of numerical methods and validation processes for predicting transitional flows based on the Langtry–Menter local correlation-based transition model, integrated with both one-equation Spalart–Allmaras (S–A) and two-equation Shear Stress Transport (SST) turbulence models. A comparative study is presented to combine the respective merits of the two coupling methods in the context of predicting the boundary-layer transition phenomenon from fundamental benchmark flows to realistic helicopter rotors. The book will of interest to industrial practitioners working in aerodynamic design and the analysis of fixed-wing or rotary wing aircraft, while also offering advanced reading material for graduate students in the research areas of Computational Fluid Dynamics (CFD), turbulence modeling and related fields.
Army R, D & A.
Author : Anonim
Publisher : Unknown
Page : 36 pages
File Size : 45,6 Mb
Release : 1980-05
Category : Military research
ISBN : UIUC:30112101565627
Army R, D & A. by Anonim Pdf
Army RD & A.
Author : Anonim
Publisher : Unknown
Page : 696 pages
File Size : 40,8 Mb
Release : 1979
Category : Military research
ISBN : CUB:U183016111607
Army RD & A. by Anonim Pdf
Army RD & A Bulletin
Author : Anonim
Publisher : Unknown
Page : 254 pages
File Size : 41,7 Mb
Release : 1980
Category : Military research
ISBN : UVA:X001765607
Army RD & A Bulletin by Anonim Pdf
Flights of Discovery
Author : Lane E. Wallace
Publisher : Unknown
Page : 214 pages
File Size : 45,5 Mb
Release : 2006
Category : Government publications
ISBN : IND:30000116800768
Flights of Discovery by Lane E. Wallace Pdf
Lecture Notes in Rotorcraft Engineering
Author : Antonio Filippone,George Barakos
Publisher : Springer Nature
Page : 255 pages
File Size : 48,6 Mb
Release : 2023-01-27
Category : Technology & Engineering
ISBN : 9783031124372
Lecture Notes in Rotorcraft Engineering by Antonio Filippone,George Barakos Pdf
This textbook is a multi-disciplinary compendium that includes several aspects of rotorcraft technology. It introduces the reader to the aerodynamic aspects of rotary wings and presents experimental techniques for aerodynamics. The chapters also cover rotorcraft engines and rotorcraft steady-state flight performance and stability. It explores several aspects of the tiltrotor configuration and lists challenges in their design, modelling and simulation. The reader will also find an introductory overview of flight control systems for rotorcraft, as well as the conceptual and preliminary design concepts for a conventional helicopter. This textbook contains video recordings of computer simulations that can be used alongside the main text.