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Important Announcement: Application Deadline Extended
New Editor-in-Chief Sought for the Journal of Propulsion and Power
Vigor Yang, current Editor-in-Chief of the Journal of Propulsion and Power, will step down from his position after 8 years of service at the end of 2009. We are seeking an outstanding candidate with an international reputation for this position, and we invite your nominations. This is an open process, and the final selection will be made only on the basis of the applicants’ merits.

The Journal of Propulsion and Power was founded in the early 1980s to promote the advancement in airbreathing, electric, and advanced propulsion, solid and liquid rockets, combustion, fuels and propellants, power generation and conversion for aerospace vehicles, and terrestrial energy devices and systems. While the original concept for the journal originated from AIAA’s Airbreathing Propulsion TC, the early exploration of the concept broadened the journal’s scope to encompass rocket technologies and basic combustion phenomena related to propulsion. Furthermore because the decision had been made to suspend publication of AIAA’s Journal of Energy, energy conversion papers were also included in the scope.

Today aerospace propulsion and power remain critical technical issues as we look for new sources of power for space exploration as well as more efficient and environmentally responsible power sources for terrestrial applications in general and aerospace vehicles in particular. JPP will be critical as the journal of record for this research. The next editor-in-chief will play a critical role in documenting the discoveries and advances to come.

The Editor-in-Chief is responsible for maintaining the quality and reputation of the journal. He or she receives manuscripts, assigns them to Associate Editors for review and evaluation, and monitors the performance of the Associate Editors to ensure that the manuscripts are processed in a fair and timely manner. The Editor-in-Chief works closely with AIAA Headquarters staff on both general procedures and the scheduling of specific issues. Detailed record keeping and prompt actions are required. The Editor-in-Chief is expected to provide his or her own clerical support, although this may be partially offset by a small expense allowance. AIAA provides a computer and a Web-based manuscript-tracking system.

Interested candidates are invited to send full résumés, including a complete list of published papers, to:

Rodger Williams
American Institute of Aeronautics and Astronautics
1801 Alexander Bell Drive, Suite 500
Reston, VA 20191-4344
Fax: 703.264.7551
E-mail: rodgerw@aiaa.org

Two letters of recommendation also are required. The recommendations should be sent by the parties writing the letters directly to Mr. Williams at the above address, fax number, or e-mail. All materials must be received at AIAA Headquarters by 30 June 2009.

A selection committee will review the applications and will recommend qualified candidates to the AIAA Vice President–Publications, who in turn will present a recommendation to the AIAA Board of Directors for approval. All candidates will be notified of the final decision.

JOURNAL OF PROPULSION AND POWER
Editor-in-Chief :
Vigor Yang

Georgia Institute of Technology
Frequency Bimonthly
ISSN 0748-4658
E-ISSN 1533-3876
CURRENT ISSUE
2009 vol. 25 no. 3

Experimental Study of a Mach 3 Bump-Compression Flowfield
pages (545-554)
doi: 10.2514/1.35306
    Benjamin J. Tillotson; Eric Loth; J Craig Dutton; James Mace; Bruce Haeffele
Shock-Tunnel Experiments with a Mach 12 Rectangular-to-Elliptical Shape-Transition Scramjet at Offdesign Conditions
pages (555-564)
doi: 10.2514/1.37946
    Milinda V. Suraweera; Michael K. Smart
Suitability of C2-, C3-Hydrocarbon Fuels for Plasma Ignition in High-Speed Flow
pages (565-570)
doi: 10.2514/1.38906
    Kenichi Takita; Ryuta Ohashi; Naoyuki Abe
Swept-Leading-Edge Pylon Effects on a Scramjet Pylon-Cavity Flameholder Flowfield
pages (571-582)
doi: 10.2514/1.39546
    Andrew B. Freeborn; Paul I. King; Mark R. Gruber
Mixing and Combustion Characteristics of Kerosene in a Model Supersonic Combustor
pages (583-592)
doi: 10.2514/1.40140
    K. Kumaran; V. Babu
Investigation of Self-Sustaining Waves in Metastable Systems: Deflagration to Detonation Transition
pages (593-608)
doi: 10.2514/1.33078
    Nickolay N. Smirnov; Valeriy F. Nikitin; Shaban Alyari Shurekhdeli
Experimental Investigation of a Novel Combustor Model for Gas Turbines
pages (609-617)
doi: 10.2514/1.35173
    Mário Costa; Mário Melo; João Sousa; Yeshayahou Levy
Adaptive Instability Suppression Controls Method For Aircraft Gas Turbine Engine Combustors
pages (618-627)
doi: 10.2514/1.36777
    George Kopasakis; John C. DeLaat; Clarence T. Chang
Performance Evaluation of a Fast Mobility-Based Particle Spectrometer for Aircraft Exhaust
pages (628-634)
doi: 10.2514/1.37654
    Donald E. Hagen; Prem Lobo; Philip D. Whitefield; Max B. Trueblood; Darryl J. Alofs; Otmar Schmid
Multiple-Point Adaptive Performance Simulation Tuned to Aeroengine Test-Bed Data
pages (635-641)
doi: 10.2514/1.38823
    Yi-Guang Li; Luca Marinai; Vassilios Pachidis; E. Lo Gatto; P. Philidis
Development and Application of an Arbitrary Lagrangian Eulerian Solver for Turbomachinery Aeromechanics
pages (642-652)
doi: 10.2514/1.36068
    Kishore Ramakrishnan; Dana Gottfried; Patrick B. Lawless; Sanford Fleeter
Experimental Investigations of Pressure Distortions on the High-Pressure Compressor Operating Behavior
pages (653-667)
doi: 10.2514/1.37412
    Niko Reuss; Christian Mundt
Shock/Boundary-Layer/Tip-Clearance Interaction in a Transonic Rotor Blade
pages (668-677)
doi: 10.2514/1.39541
    Roberto Biollo; Ernesto Benini
Flow Characteristics of Tip Injection on Compressor Rotating Spike via Time-Accurate Simulation
pages (678-687)
doi: 10.2514/1.41428
    Jen-Ping Chen; Benjamin P. Johnson; Michael D. Hathaway; Robert S. Webster
Experimental and Numerical Study of Jet Mixing from a Shock-Containing Nozzle
pages (688-696)
doi: 10.2514/1.37022
    Qing Xiao; Her Mann Tsai; Dimitri Papamoschou; Andrew Johnson
Optimization of Second Throat Ejectors for High-Altitude Test Facility
pages (697-706)
doi: 10.2514/1.39219
    Manikanda R. Kumaran; Vivekanand P. Kumaresan; T. Sundararajan; Kumaresan K.; Raja D. Manohar
Compressible Flow Structures Interaction with a Two-Dimensional Ejector: A Cold-Flow Study
pages (707-716)
doi: 10.2514/1.39315
    Konstantinos Kontis; Hossein Zare-Behtash
Design of Quiet Propeller for an Electric Mini Unmanned Air Vehicle
pages (717-728)
doi: 10.2514/1.38814
    Ohad Gur; Aviv Rosen
Thrust Measurement of the Hybrid Electric Thruster TIHTUS by a Baffle Plate
pages (729-736)
doi: 10.2514/1.34324
    Hannah Böhrk; Monika Auweter-Kurtz
Plume Profiles of a Planar Crossed-Field Thruster with Hall Current Injection
pages (737-745)
doi: 10.2514/1.35720
    Joshua L. Rovey; Matthew Giacomi; Robert Stubbers; Brian Jurczyk
Validating a Plasma Momentum Flux Sensor to an Inverted Pendulum Thrust Stand
pages (746-752)
doi: 10.2514/1.35706
    Benjamin W. Longmier; Bryan M. Reid; Alec D. Gallimore; Franklin R. Chang-Diaz; Jared P. Squire; Tim W. Glover; Greg Chavers; Edgar A. Bering
Ground Test Investigation of Temperature Distribution in Four Parallel High-Altitude Engines
pages (753-759)
doi: 10.2514/1.38313
    Wen Bo Qin; Hui Er Cheng; Peng Li
Circumferential Film Cooling Effectiveness in a LOX/H2 Subscale Combustion Chamber
pages (760-770)
doi: 10.2514/1.40305
    Richard Arnold; Dmitry Suslov; Oskar Haidn
Computational Analysis of the Oxidizer Preflow in an Upper-Stage Rocket Engine
pages (771-782)
doi: 10.2514/1.38309
    Roland Schmehl; Johan Steelant
Performance Characteristics of an Annular Conical Aerospike Nozzle with Freestream Effect
pages (783-791)
doi: 10.2514/1.40302
    Shashi Bhushan Verma
Passive Control of Pressure Oscillations in Solid Rocket Motors: Cold-Flow Experiments
pages (792-800)
doi: 10.2514/1.39794
    Jerome Anthoine; Marcos R. Lema
Pyrolysis/Evaporation Study of Succinic Acid/Polyvinyl Acetate for Reducing Nozzle Throat Erosion
pages (801-807)
doi: 10.2514/1.37508
    Kenneth K. Kuo; Ragini Acharya; Eric Boyd; Stefan Thynell
Flame-Spreading Behavior in a Fin-Slot Solid Propellant Rocket Motor Grain (Part II)
pages (808-814)
doi: 10.2514/1.38166
    Jeffrey D. Moore; Kenneth K. Kuo; Peter J. Ferrara
Predicting Hybrid Propellant Regression Rate Using Response Surfaces
pages (815-818)
doi: 10.2514/1.14418
    Robert A. Frederick; Joshua J. Whitehead
Buzz Instability in a Mixed-Compression Air Intake
pages (819-822)
doi: 10.2514/1.39751
    P. Vivek; Sanjay Mittal
Development of a Specific Impulse Balance for Capillary Discharge Pulsed Plasma Thrusters
pages (823-826)
doi: 10.2514/1.40261
    Taylor C. Lilly; Andrew Ketsdever; Anthony P. Pancotti; Marcus Young
Condensation-Induced Surface Boiling of Alcohol Fuel Droplets in Combustion Chambers
pages (826-828)
doi: 10.2514/1.40544
    Daniel E. Rosner; Manuel Arias-Zugasti
Liquid Monopropellant Combustion in Mesoscale Vortex Chamber
pages (829-832)
doi: 10.2514/1.40662
    Ming-Hsun Wu; Yanxing Wang; Richard A. Yetter; Vigor Yang
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