Author: Helmut F. ButzePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
Book Description
Parametric Performance of a Turbojet Engine Combustor Using Jet A and A Diesel Fuel
Author: Helmut F. ButzePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
Book Description
Parametric Performance Evaluation of a Jet Engine Derived from a Turbocharger
Author: Richard B. BrownPublisher:
ISBN:
Category :
Languages : en
Pages : 118
Book Description
Previous conceptual studies have shown that it is feasible to construct a low-thrust, jet engine, based on a production turbocharger at relatively low cost. A parametric evaluation was performed on a turbojet engine derived from an AiResearch 1.5 lb(m)/sec airflow turbocharger unit to determine its static performance characteristics and the maximum attainable thrust without augmentation or major component modification. The performance of various turbine housing/nozzle combinations was measured in steady state operation using a much improved instrumentation system, together with various system improvements. Parameters were measured on a common time base and plotted to depict the total performance of the unit over its usable range. Maximum thrust obtained was 97 lb(f), exceeding the initially predicted theoretical value of 67 lb(f) by 45%. Data was reduced to coded 3 digit numbers for programming and plotting using the CDC 6600 computer. The results were machine plots depicting the performance characteristics of the unaugmented engine for use in further studies including augmentation. In addition, computer performance programs for coded raw data were written for future data reduction and analysis. (Author).
Effect of Fuel Properties on Performance of Single Aircraft Turbojet Combustor at Simulated Idle, Cruise, and Takeoff Conditions
Author: Helmut F. ButzeGas Turbine Performance
Author: Philip P. WalshPublisher: John Wiley & Sons
ISBN: 140515103X
Category : Technology & Engineering
Languages : en
Pages : 664
Book Description
A significant addition to the literature on gas turbine technology, the second edition of Gas Turbine Performance is a lengthy text covering product advances and technological developments. Including extensive figures, charts, tables and formulae, this book will interest everyone concerned with gas turbine technology, whether they are designers, marketing staff or users.
NASA SP.
Author: Energy
Author: Aeronautical Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Scientific and Technical Aerospace Reports
Author: Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components
Author: Carl E. CampbellPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
Compressor performance and turbine performance are presented in the form of performance maps at selected values of Reynolds number index; the effects of Reynolds number on performance are summarized. The effects of variable stator angle and high inlet-air temperatures on compressor performance are also shown. Over-all engine performance (net thrust and specific fuel consumption) is presented for a flight Mach number of 0.9 at rated engine conditions over a range of altitudes to illustrate performance losses resulting from decreased Reynolds number index.
Author: