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SCIENTIFIC AND TECHNICAL AEROSPACE REPORTS

NASA STAR REPORTS: 07/05/06
Aeronautics

02 Aerodynamics

03 Air Transportation and Safety

04 Aircraft Communications and Navigation

05 Aircraft Design, Testing and Performance

07 Aircraft Propulsion and Power

08 Aircraft Stability and Control

09 Research and Support Facilities (Air)

07 AIRCRAFT PROPULSION AND POWER
Includes primary propulsion systems and related systems and components, e.g., gas turbine engines, compressors, and fuel systems; and onboard auxiliary power plants for aircraft.

For related information see also 20 Spacecraft Propulsion and Power; 28 Propellants and Fuels; and 44 Energy Production and Conversion.


20060016613 Innovative Scientific Solutions, Inc., Dayton, OH USA

Detonation Initiation Studies and Performance Results for Pulsed Detonation Engine Applications

Schauer, Fred; Stutrud, Jeff; Bradley, Royce; Jan 2001; 11 pp.; In English; Original contains color illustrations Report No.(s): AD-A444161; AIAA-2001-1129; No Copyright; ONLINE: http://hdl.handle.net/100.2/ADA444161; Avail.: CASI: A03, Hardcopy

An in-house computational and experimental program to investigate and develop an air breathing pulse detonation engine (PDE) that uses a practical fuel (kerosene based, fleet-wide use, JP type) is currently underway at the Combustion Sciences Branch of the Turbine Engine Division of the Air Force Research Laboratory (AFRL/PRTS). PDE's have the potential of high thrust, low weight, low cost, high scalability, and wide operating range, but several technological hurdles must be overcome before a practical engine can be designed.

This research effort involves investigating such critical issues as: detonation initiation and propagation; valving, timing and control; instrumentation and diagnostics; purging, heat transfer, and repetition rate; noise and multi-tube effects; detonation and deflagration to detonation transition modeling; and performance prediction and analysis. An innovative, four-detonation-tube engine design is currently in test and evaluation. Preliminary data are obtained with premixed hydrogen/air as the fuel/oxidizer to demonstrate proof of concept and verify models. Techniques for initiating detonations in hydrogen/air mixtures are developed without the use of oxygen enriched air. An overview of the AFRL/PRTS PDE development research program and hydrogen/air results are presented. DTIC

Air Breathing Engines; Detonation Waves; Initiation; Pulse Detonation Engines

Source: NASA


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