Supersonic Transport Development Program. Phase Iii Proposal. Boeing Model 2707. Volume Ii-4. Airplane Performance (general Electric). PDF Download
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Author: Clarence S Howell (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 162
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Book Description
Contents: Flight Limits; Takeoff; Climb; Cruise; Descent; Holding and Reserves; Landing; Off-Design Versatility; Trade Data; and Weights.
Author: Clarence S Howell (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 162
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Book Description
Contents: Flight Limits; Takeoff; Climb; Cruise; Descent; Holding and Reserves; Landing; Off-Design Versatility; Trade Data; and Weights.
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 117
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Book Description
Throughout Phase II-C, as in earlier phases of the SST Program, The Boeing Company has maintained a program of design analysis and performance evaluation, with the coordinated participation of both engine contractors. As a result, the General Electric GE4/J5P powered B-2707 (GE) and the Pratt and Whitney Aircraft JFT17A-21B powered B-2707 (P and WA) airplanes are very competitive in terms of overall airplane performance criteria, and either would make an outstanding airline airplaned. The purpose of this document is to report the technical evaluation of the two engines. Considerations in this evaluation include engine/airplane matching and performance, engine design, installation compatibility, development plan, development risk, and growth potential.
Author: Clarence S Howell (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 174
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Book Description
Performance data are presented for the Boeing Model B-2707 (P and WA) intercontinental and domestic supersonic transports. Complete data are given to show the effects of weight, speed, altitude, power setting, and temperature so that airline operational and route analysis studies may be made. These data augment the basic performance given in Aerodynamic Design Report, V2-B2707-3.
Author: BOEING CO SEATTLE WASH SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 308
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Book Description
This document includes the summary and three major sections of the propulsion report describing the engines, supersonic inlet, and the propulsion control systems. Studies conducted during Phase II C have resulted in significant improvements to the Boeing Model 2707 propulsion system. Optimum sized engines with improved thrust and fuel consumption characteristics are available from General Electric and Pratt and Whitney Aircraft. The four separate and interchangeable propulsion pods are mounted below the lower surface of the horizontal stabilizer at such a position that the engine exhaust will not impinge on any part of the airplane. The pod location and shape provides optimum lift effect on the airplane.
Author: James W. McKee
Publisher:
ISBN:
Category :
Languages : en
Pages : 237
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Book Description
The air-conditioning system includes a cabin air source and associated cooling equipment, passenger cabin and flight deck air distribution and exhaust system, cabin temperature control, cabin pressure control, equipment and compartment conditioning, and instruments to monitor ozone levels. The adverse weather systems include ice and fog protection and rain removal for the flight deck windshields. Fog protection is provided for the movable-nose side windows. Ice protection is provided for the engine inlets and air data sensors. The oxygen system includes a gaseous oxygen system for the flight crew members and portable first-air oxygen units for the passenger cabin occupants and flight crew members. The electrical system comprises all electrical equipment required for generation, control, conversion, storage, and distribution of electrical power. It also includes electrical and electronic wiring and circuit protection devices between the distribution buses and the utilization loads and the airplane internal and external lights. Radio navigation and communication design and performance requirements have generally been well-established through action by airline industry study groups; e.g. RTCA, ATA, ARINC, and are therefore discussed briefly. Inertial Navigation and Weather Radar are development items, not yet fully defined, and are discussed in detail.
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 784
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Book Description
Author: D. M. Petrie
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Book Description
The Flight Simulation Program discussed herein is an element in the total test documentation. Flight simulations are characteristically different from other simulations in that the work is primarily addressed to the development of systems, including the man machine relationship, that control the flight path of the airplane and to performance evaluation of the dynamic behavior of the airplane in flight in its simulated environment. Another identifying feature is that computers are used to simulate in real time the mathematical relationships between the disturbing forces and the control forces applied to the airplane and, in many cases, the control system hardware. Airplane performance and design studies which utilize analog and digital computers, (generally open loop and not necessarily real time) are not considered to be within the scope of flight simulation. The purpose of the flight simulation program is to aid in the development and integration of those subsystems that are required for safe and efficient flight-path control of the airplane; assist in the evaluation of the effects on the flight dynamics of the fluid environment through which the airplane will fly; determine the operational margins in both normal and abnormal operating conditions; and contribute to the training of the flight test crews. The results of the flight simulation program will be a factor in the development of an airplane, along with associated operating procedures, that are compatible with the airline operational environment.
Author: C. S. Howell
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
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Book Description
The calculation of sonic boom characteristics of the Boeing Model 2707 is described; configuration geometry and pertinent aerodynamic data are detailed in the Aerodynamic Design Document, V2-B2707-3; sonic boom data, as related to airplane performance, are presented in the Airline Performance-GE, and Airline Performance-P and W Documents, V2-B2707-4 and -5. Consideration of sonic boom has been fundamental in the design of the B-2707. The configuration has been optimized to obtain the best sonic boom characteristics at all Mach numbers, commensurate with minimum drag, and structural weight considerations. This is evidenced by the fact that despite increases in fuselage size for improved passenger accommodations, the airplane essentially meets the FAA objectives for domestic and international operations.
Author: D. R. Donaldson
Publisher:
ISBN:
Category :
Languages : en
Pages : 226
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Book Description
A comprehensive development and verification test program has been established for the structure of the B-2707 airplane. It recognizes the more demanding usage and environment to which the airplane is subjected, and the use of relatively new structural materials and processes. Additionally, it recognizes the problems of contemporary airplanes and provides testing of proper magnitude and timing to preclude recurrence of similar problems on the SST. Structural areas of concern have been covered by systematic development tests to provide the maximum information possible prior to final design. Toward this end, Boeing has conducted development tests of the SST structure and materials to establish reliable strength, fatigue life, and fail-safe concepts continuously during the past 8-years.
Author: BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV.
Publisher:
ISBN:
Category :
Languages : en
Pages : 52
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Book Description
Contents: Flight Test Integration and Management; Phase III Prototype Flight Test, 100-FLIGHT Hour Evaluation; Phase IV Flight Test Program; Phase V - Production Airplane Acceptance; Test Instrumentation and Data System; Test Facilities; Test Equipment; and Phase II-C and Phase III Flight Test Preparation Activities.
