WorldCat Identities

Boeing Commercial Airplane Company

Overview
Works: 578 works in 840 publications in 1 language and 5,222 library holdings
Classifications: TL521.3.C6, 629.135
Publication Timeline
Key
Publications about Boeing Commercial Airplane Company Publications about Boeing Commercial Airplane Company
Publications by Boeing Commercial Airplane Company Publications by Boeing Commercial Airplane Company
Most widely held works about Boeing Commercial Airplane Company
 
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Most widely held works by Boeing Commercial Airplane Company
Performance of a commercial transport under typical MLS noise environment final report by John K Ho ( )
4 editions published in 1986 in English and held by 221 WorldCat member libraries worldwide
Integrated application of active controls (IAAC) technology to an advanced subsonic transport project program review ( Book )
2 editions published between 1982 and 1986 in English and held by 150 WorldCat member libraries worldwide
An experimental study of airfoil-spoiler aerodynamics by Joint Institute for Aeronautics and Acoustics ( )
1 edition published in 1984 in English and held by 149 WorldCat member libraries worldwide
A conflict analysis of 4D descent strategies in a metered, multiple-arrival route environment by K. H Izumi ( Book )
1 edition published in 1990 in English and held by 116 WorldCat member libraries worldwide
Terminal configured vehicle program : test facilities guide by Langley Research Center ( Book )
5 editions published in 1980 in English and held by 98 WorldCat member libraries worldwide
IPAD user requirements implementation (first-level IPAD), D6-IPAD-70016-D-1 ( Book )
1 edition published in 1980 in English and held by 85 WorldCat member libraries worldwide
Study to determine potential flight applications and human factors design guidelines for voice recognition and synthesis systems final report by Russell W White ( Book )
2 editions published in 1985 in English and held by 80 WorldCat member libraries worldwide
A study was conducted to determine potential commercial aircraft flight deck applications and implementation guidelines for voice recognition and synthesis. At first, a survey of voice recognition and synthesis technology was undertaken to develop a working knowledge base. Then, numerous potential aircraft and simulator flight deck voice applications were identified and each proposed application was rated on a number of criteria in order to achieve an overall payoff rating. The potential voice recognition applications fell into five general categories: programming, interrogation, data entry, switch and mode selection, and continuous/time-critical action control. The ratings of the first three categories showed the most promise of being beneficial to flight deck operations. Possible applications of voice synthesis systems were categorized as automatic or pilot selectable and many were rated as being potentially beneficial. In addition, voice system implementation guidelines and pertinent performance criteria are proposed. Finally, the findings of this study are compared with those made in a recent NASA study of a 1995 transport concept
Specification for a Program for an Iterative Aeroelastic Solution (PIAS) ( Book )
2 editions published in 1983 in English and held by 79 WorldCat member libraries worldwide
Development of quality assurance methods for epoxy graphite prepreg by J. S Chen ( Book )
3 editions published in 1982 in English and held by 76 WorldCat member libraries worldwide
The objective of this program was to develop quality assurance methods for graphite epoxy/prepregs. Liquid chromatography, differential scanning calorimetry, and gel permeation chromatography were investigated. These methods were applied to a second prepreg system. The program also sought to correlate the resin matrix formulation with mechanical properties. Dynamic mechanical analysis and fracture toughness methods were investigated. Liquid chromatography, differential scanning calorimetry, and gel permeation chromatography were all successfully developed as quality assurance methods for graphite epoxy prepregs. The liquid chromatography method was the most sensitive to changes in resin formulation. All three methods were successfully applied to a second prepreg system. No correlation could be established between mechanical properties and the resin formulation variations defined within this contract
Electrical insulation fire characteristics ( Book )
3 editions published between 1978 and 1983 in English and held by 74 WorldCat member libraries worldwide
A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils by Edward F Ehlers ( Book )
3 editions published in 1982 in English and held by 73 WorldCat member libraries worldwide
Study of supersonic wings employing the attainable leading-edge thrust concept by W. D Middleton ( Book )
3 editions published in 1982 in English and held by 72 WorldCat member libraries worldwide
Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies by Theodore A Reyhner ( Book )
3 editions published in 1982 in English and held by 72 WorldCat member libraries worldwide
Systems study for an Integrated Digital/Electric Aircraft (IDEA) by G. E Tagge ( Book )
3 editions published in 1985 in English and held by 71 WorldCat member libraries worldwide
The results of the Integrated Digital/Electric Aircraft (IDEA) Study are presented. Airplanes with advanced systems were, defined and evaluated, as a means of identifying potential high payoff research tasks. A baseline airplane was defined for comparison, typical of a 1990's airplane with advanced active controls, propulsion, aerodynamics, and structures technology. Trade studies led to definition of an IDEA airplane, with extensive digital systems and electric secondary power distribution. This airplane showed an improvement of 3% in fuel use and 1.8% in DOC relative to the baseline configuration. An alternate configuration, an advanced technology turboprop, was also evaluated, with greater improvement supported by digital electric systems. Recommended research programs were defined for high risk, high payoff areas appropriate for implementation under NASA leadership
Evaluation of analysis techniques for low frequency interior noise and vibration of commercial aircraft by A. E Landmann ( Book )
3 editions published in 1989 in English and held by 71 WorldCat member libraries worldwide
Development of integrated programs for aerospace-vehicle design (IPAD), product program management systems by J. M Isenberg ( Book )
3 editions published in 1979 in English and held by 70 WorldCat member libraries worldwide
A method for computing the leading-edge suction in a highr-order panel method by F. Edward Ehlers ( Book )
2 editions published in 1984 in English and held by 69 WorldCat member libraries worldwide
A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLEX) by M Richard ( Book )
2 editions published in 1979 in English and held by 69 WorldCat member libraries worldwide
The program input presented consists of configuration geometry, aerodynamic parameters, and modal data; output includes element geometry, pressure difference distributions, integrated aerodynamic coefficients, stability derivatives, generalized aerodynamic forces, and aerodynamic influence coefficient matrices. Optionally, modal data may be input on magnetic file (tape or disk), and certain geometric and aerodynamic output may be saved for subsequent use.--V. I. The information necessary for execution of the digital computer program L216 on the CDC 6600 is described. L216 characteristics are based on the doublet lattice method. Arbitrary aerodynamic configurations may be represented with combinations of nonplanar lifting surfaces composed of finite constant pressure panel elements, and axially summetric slender bodies composed of constant pressure line elements. Program input consists of configuration geometry, aerodynamic parameters, and modal data; output includes element geometry, pressure difference distributions, integrated aerodynamic coefficients, stability derivatives, generalized aerodynamic forces, and aerodynamic influence coefficient matrices. Optionally, modal data may be input on magnetic field (tape or disk), and certain geometric and aerodynamic output may be saved for subsequent use.--V. II
Study of metallic structural design concepts for an arrow wing supersonic cruise configuration by M. J Turner ( Book )
2 editions published in 1977 in English and held by 68 WorldCat member libraries worldwide
Integrated application of active controls (IAAC) technology to an advanced subsonic transport project test ACT system description ( Book )
1 edition published in 1983 in English and held by 68 WorldCat member libraries worldwide
 
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Alternative Names

controlled identity Boeing Commercial Airplanes

controlled identity Boeing Company. Commercial Airplane Group

Boeing Company. Boeing Commercial Airplane Company
Boeing Company. Commercial Airplane Company
Languages
English (72)
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