Welcome to our book review site go-pdf.online!

You may have to Search all our reviewed books and magazines, click the sign up button below to create a free account.

Sign up

NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, *
  • Language: en
  • Pages: 1070
NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research
  • Language: en
  • Pages: 1064

NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research

  • Type: Book
  • -
  • Published: 2010
  • -
  • Publisher: Unknown

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.

Innovation in Flight
  • Language: en
  • Pages: 406

Innovation in Flight

  • Type: Book
  • -
  • Published: 2005
  • -
  • Publisher: Unknown

None

Piloted Simulation Assessment of a High-Speed Civil Transport Configuration
  • Language: en
  • Pages: 484

Piloted Simulation Assessment of a High-Speed Civil Transport Configuration

  • Type: Book
  • -
  • Published: 2002
  • -
  • Publisher: Unknown

An assessment of a proposed configuration of a high-speed civil transport was conducted by using NASA and industry research pilots. The assessment was conducted to evaluate operational aspects of the configuration from a pilot's perspective, with the primary goal being to identify potential deficiencies in the configuration. The configuration was evaluated within and at the limits of the design operating envelope to determine the suitability of the configuration to maneuver in a typical mission as well as in emergency Or envelope-limit conditions. The Cooper-Harper rating scale was used to evaluate the flying qualities of the configuration. A summary flying qualities metric was also calculated. The assessment was performed in the Langley six-degree-of-freedom Visual Motion Simulator. The effect of a restricted cockpit field-of-view due to obstruction by the vehicle nose was not included in this study.

Human Factors in Aviation
  • Language: en
  • Pages: 747

Human Factors in Aviation

Fully updated and expanded, the second edition of Human Factors in Aviation serves the needs of the widespread aviation community - students, engineers, scientists, pilots, managers and government personnel. Offering a comprehensive overview the volume covers topics such as pilot performance, human factors in aircraft design, vehicles and systems and NextGen issues. The need for an up-to-date, scienti?cally rigorous overview is underscored by the frequency with which human factors/crew error cause aviation accidents, pervasiveness of human error in safety breakdowns. Technical and communication advances, diminishing airspace and the priority of aviation safety all contribute to the generation of new human factors problems and the more extensive range of solutions. Now more than ever a solid foundation from which to begin addressing these issues is needed. - New edition thoroughly updated with 50% new material, offering full coverage of NexGen and other modern issues - Liberal use of case examples exposes students to real-world examples of dangers and solutions - Website with study questions and image collection

Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport
  • Language: en
  • Pages: 98

Simulation Study of Impact of Aeroelastic Characteristics on Flying Qualities of a High Speed Civil Transport

  • Type: Book
  • -
  • Published: 2002
  • -
  • Publisher: Unknown

A piloted simulation study conducted in NASA Langley Visual Motion Simulator addressed the impact of dynamic aero- servoelastic effects on flying qualities of a High Speed Civil Transport. The intent was to determine effectiveness of measures to reduce the impact of aircraft flexibility on piloting tasks. Potential solutions examined were increasing frequency of elastic modes through structural stiffening, increasing damping of elastic modes through active control, elimination of control effector excitation of the lowest frequency elastic modes, and elimination of visual cues associated with elastic modes. Six test pilots evaluated and performed simulated maneuver tasks, encountering incidents wherein cockpit vibrations due to elastic modes fed back into the control stick through involuntary vibrations of the pilots upper body and arm.

On Subscale Flight Testing
  • Language: en
  • Pages: 130

On Subscale Flight Testing

Downscaled physical models, also referred to as subscale models, have played an essential role in the investigation of the complex physics of flight until the recent disruption of numerical simulation. Despite the fact that improvements in computational methods are slowly pushing experimental techniques towards a secondary role as verification or calibration tools, real-world testing of physical prototypes still provides an unmatched confidence. Physical models are very effective at revealing issues that are sometimes not correctly identified in the virtual domain, and hence can be a valuable complement to other design tools. But traditional wind-tunnel testing cannot always meet all of the ...

Monthly Catalogue, United States Public Documents
  • Language: en
  • Pages: 1064

Monthly Catalogue, United States Public Documents

  • Type: Book
  • -
  • Published: 1994
  • -
  • Publisher: Unknown

None

Piloted Simulation Study of an ILS Approach of a Twin-pusher Business/commuter Turboprop Aircraft Configuration
  • Language: en
  • Pages: 128

Piloted Simulation Study of an ILS Approach of a Twin-pusher Business/commuter Turboprop Aircraft Configuration

  • Type: Book
  • -
  • Published: 1994
  • -
  • Publisher: Unknown

A six-degree-of-freedom nonlinear simulation of a twin-pusher, turboprop business/commuter aircraft configuration representative of the Cessna ATPTB (Advanced turboprop test bed) was developed for use in piloted studies with the Langley General Aviation Simulator. The math models developed are provided, simulation predictions are compared with with Cessna flight-test data for validation purposes, and results of a handling quality study during simulated ILS (instrument landing system) approaches and missed approaches are presented. Simulated flight trajectories, task performance measures, and pilot evaluations are presented for the ILS approach and missed-approach tasks conducted with the vehicle in the presence of moderate turbulence, varying horizontal winds and engine-out conditions. Six test subjects consisting of two research pilots, a Cessna test pilot, and three general aviation pilots participated in the study. This effort was undertaken in cooperation with the Cessna Aircraft Company.