3 edition of Advanced methods of structural and trajectory analysis for transport aircraft found in the catalog.
Advanced methods of structural and trajectory analysis for transport aircraft
Mark D. Ardema
Published
1995
by Santa Clara University, National Aeronautics and Space Administration, National Technical Information Service, distributor in Santa Clara, CA, [Washington, DC, Springfield, Va
.
Written in English
Edition Notes
| Statement | Mark D. Ardema, principal investigator. |
| Series | NASA contractor report -- NASA CR-199949. |
| Contributions | United States. National Aeronautics and Space Administration. |
| The Physical Object | |
|---|---|
| Format | Microform |
| Pagination | 1 v. |
| ID Numbers | |
| Open Library | OL15425853M |
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Get this from a library. Advanced methods of structural and trajectory analysis for transport aircraft: final report, J - Septem [Mark D Ardema; United States. National Aeronautics and Space Administration.].
Get this from a library. Development of advanced methods of structural and trajectory analysis for transport aircraft: final report: October 1, Febru NASA Ames Research Center grant NCC [Mark D Ardema; United States. National Aeronautics and.
Advanced Methods of Structural and Trajectory Analysis for Transport Aircraft. This book is an extension of the authorâ s basic book on Structural Analysis.
The initial three chapters review the basic concepts in structural analysis and matrix algebra, and show how the latter provides an excellent mathematical framework for the former. Development of advanced methods of structural and trajectory analysis for transport aircraft.
Technical Report CR, NASA, Mar. ADVANCED AIRCRAFT FLIGHT PERFORMANCE mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of environ-mental performance. A unique feature of this book is the discussion Drag Analysis of Transport Aircraft Case Study: Drag Analysis of the ATR A unique feature of this book is the discussion and analysis of the environmental performance of the aircraft, focusing on topics such as aircraft noise and Author: Antonio Filippone.
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This report summarizes the efforts in two areas: (1) development of advanced methods of structural weight estimation, and (2) development of advanced methods of trajectory optimization.
Aircraft Functional Hazard Assessment of Transport Aircraft. This book takes a two engine transport aircraft as an example. The aircraft is designed to carry 75 passengers with an average cruising speed of Mach, a maximum range of nautical miles, an average flight duration of hours, and a 50,hour service life.
The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of Author: Ajoy Kumar Kundu.
Performance of the Jet Transport Airplane: Analysis Methods, Flight Operations, and Regulations. presents a detailed and comprehensive treatment of performance analysis techniques for jet transport airplanes.
Uniquely, the book describes key operational and regulatory procedures and constraints that directly impact the performance of commercial. Examples in this group include ejector rockets, high Mach carrier aircraft, aerostats, vertical jet boosters, and low-G gas accelerators.
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The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of Author: Antonio Filippone.
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First let it be assumed that a simplifying assumption for confirming or estimating the value of drag constant, k, is to assume that k is a function of (i) the trajectory maximum flight height, h p, Fig.(ii) the horizontal distance, L p, where the maximum height occurs, (iii) the difference in height between the ball launch point and the.
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This is achieved through aircraft servicing. The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of Author: Antonio Filippone.
An extended version of the Collar’s triangle shown in Figure 1 highlights the physical phenomena that need to be integrated for accurate modelling and simulation of flexible aircraft. Traditionally the flight dynamics community has focused on the link between inertial dynamics and aerodynamics and it assumes structural dynamics to occur at far higher frequencies than Cited by: 3.
Flight Performance of Fixed and Rotary Wing Aircraft. Publication: Elsevier, May Author: A Filippone. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes.In addition, this book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control ed Control of Aircraft, Spacecraft and Rockets features worked examples and problems at the end of each chapter as well as a number of MATLAB.• Aerodynamic design, analysis, and wind-tunnel testing of a vertical axis wind turbine.
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