Flight and Simulation Investigation of Methods for Implementing Noise abatement Landing Approaches

Flight and Simulation Investigation of Methods for Implementing Noise abatement Landing Approaches
Author: Anonim
Publsiher: Unknown
Total Pages: 132
Release: 1970
Genre: Airplanes
ISBN: UIUC:30112106780379

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Progress on NASA Research Relating to Noise Alleviation of Large Subsonic Jet Aircraft

Progress on NASA Research Relating to Noise Alleviation of Large Subsonic Jet Aircraft
Author: United States. National Aeronautics and Space Administration
Publsiher: Unknown
Total Pages: 698
Release: 1968
Genre: Airplanes
ISBN: NASA:31769000653769

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NASA Technical Note

NASA Technical Note
Author: Anonim
Publsiher: Unknown
Total Pages: 912
Release: 1971
Genre: Aeronautics
ISBN: UOM:39015006099199

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Federal Register

Federal Register
Author: Anonim
Publsiher: Unknown
Total Pages: 2508
Release: 1975
Genre: Delegated legislation
ISBN: UCR:31210024962845

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Noise Control Act Extension

Noise Control Act Extension
Author: United States. Congress. House. Committee on Interstate and Foreign Commerce. Subcommittee on Transportation and Commerce
Publsiher: Unknown
Total Pages: 108
Release: 1975
Genre: Noise control
ISBN: UOM:39015078708024

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A Piloted Simulator Investigation of Ground Effect on the Landing Maneuver of a Large Tailless Delta wing Airplane

A Piloted Simulator Investigation of Ground Effect on the Landing Maneuver of a Large  Tailless  Delta wing Airplane
Author: C. Thomas Snyder,Fred J. Drinkwater,A. David Jones
Publsiher: Unknown
Total Pages: 60
Release: 1970
Genre: Airplanes
ISBN: UIUC:30112106880864

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The influence of ground effect on the landing flare characteristics of a supersonic transport airplane (SST) was investigated in a fixed cockpit simulator. Simulations of an ogee-modified delta-wing F5D-1 airplane and a subsonic jet transport were used for evaluating the simulator and as a reference configurations during landing comparisons. Dynamic responses of the SST to seven different ground-effect models during controls-fixed and constant-attitude descents are also presented, followed by piloted subjective assessments. A summary of ground effects on delta-like wings is included in the appendixes.

Noise Control Act Extension Hearings Before the Subcommittee on Transportation and Commerce of 94 1 Mar 24 and 25 1975

Noise Control Act Extension  Hearings Before the Subcommittee on Transportation and Commerce of      94 1  Mar  24 and 25  1975
Author: United States. Congress. House. Committee on Interstate and Foreign Commerce
Publsiher: Unknown
Total Pages: 124
Release: 1975
Genre: Electronic Book
ISBN: STANFORD:36105045434862

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Criteria for Low Speed Longitudinal Handling Qualities

Criteria for Low Speed Longitudinal Handling Qualities
Author: H.A. Mooij
Publsiher: Springer Science & Business Media
Total Pages: 151
Release: 2013-04-18
Genre: Technology & Engineering
ISBN: 9789401711937

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In-fl ight simulation experiments performed in 1967 with a variable-stabil ity aircraft during the author's stay at Princeton University, motivated the study of handl ing characteristics of future transport aircraft with closed-loop fl ight control systems. In 1972, the first experiment took place at the National Aerospace Laboratory NLR, using one of its research aircraft. In anticipation of expected developments in (digital) fl ight control technology, the research programme following the first experiments was aimed at the establ ishment of quantitative handl ing qual ities criteria. An appreciable part of that programme has been sponsored by the Netherlands Agency for Aerospace Programs (Nederlands Instituut voor VI iegtuigontwikkel ing en Ruimtevaart) and the Department of Civil Aviation of the Netherlands (Rijksluchtvaartdienst). In 1981, a thorough review of the extensive and valuable data gathered was started. The result, presented in this book, was also included in the author's thesis for a Ph.D. degree of the Delft University of Technology. To introduce the reader to the multi-discipl inary field of handl ing qual ities research, introductory chapters are presented on longitudinal aircraft dynamics, closed-loop fl ight control systems using non-mechanical signal transmission, human pilot dynamics, hand I ing qual ities assessment techniques, and the present status of handl ing qual ity criteria.