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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 AIRCRAFT
Editor-in-Chief :
Thomas M. Weeks

Universal Technology Corporation
Frequency Bimonthly
ISSN 0021-8669
E-ISSN 1533-3868
CURRENT ISSUE
2009 vol. 46 no. 3

Review of Smoke Toxicity of Fiber-Polymer Composites Used in Aircraft
pages (737-745)
doi: 10.2514/1.36472
    A. P. Mouritz
Detached-Eddy Simulations of Vortex Breakdown over a 70-Degree Delta Wing
pages (746-755)
doi: 10.2514/1.4659
    Scott Morton
Pitch Stability Analysis of an Airfoil in Ground Effect
pages (756-762)
doi: 10.2514/1.31246
    Gerald M. Angle; Brian M. O'Hara; Franz A. Pertl; James E. Smith
Optimized Measurements of Unmanned-Air-Vehicle Mass Moment of Inertia with a Bifilar Pendulum
pages (763-775)
doi: 10.2514/1.34015
    Matt R. Jardin; Eric R. Mueller
Two-Level Multifidelity Design Optimization Studies for Supersonic Jets
pages (776-790)
doi: 10.2514/1.34362
    Seongim Choi; Juan J. Alonso; Ilan M. Kroo
Vibration and Flutter Characteristics of a Folding Wing
pages (791-799)
doi: 10.2514/1.34685
    Matthew P. Snyder; Brian Sanders; Franklin E. Eastep; Geoffrey J. Frank
Nonlinear Ten-Degree-of-Freedom Dynamics Model of a Generic Hypersonic Vehicle
pages (800-813)
doi: 10.2514/1.35644
    Richard Colgren; Shahriar Keshmiri; Maj Mirmirani
Structural Analysis and Testing of an Ultralight Unmanned-Aerial-Vehicle Carbon-Composite Wing
pages (814-820)
doi: 10.2514/1.36415
    R. Warsi Sullivan; Y. Hwang; M. Rais-Rohani; T. Lacy
Nonlinear Dynamic Response Structural Optimization of a Joined-Wing Using Equivalent Static Loads
pages (821-831)
doi: 10.2514/1.36762
    Y. I. Kim; G. J. Park; R. M. Kolonay; M. Blair; R. A. Canfield
Three-Dimensional Obstacle Avoidance Strategies for Uninhabited Aerial Systems Mission Planning and Replanning
pages (832-846)
doi: 10.2514/1.37244
    Franco Persiani; Francesca De Crescenzio; Giovanni Miranda; Tiziano Bombardi; Marco Fabbri; Fabio Boscolo
Single Dielectric Barrier Discharge Plasma Actuators for Improved Airfoil Performance
pages (847-855)
doi: 10.2514/1.37638
    James H. Mabe; Frederick T. Calkins; B. Wesley; R. Woszidlo; L. Taubert; I. Wygnanski
Effect of Submerged Vortex Generators on Shock-Induced Separation in Supersonic Flow
pages (856-863)
doi: 10.2514/1.37678
    A. Zare Shahneh; F. Motallebi
Plasma Flaps and Slats: An Application of Weakly Ionized Plasma Actuators
pages (864-873)
doi: 10.2514/1.38232
    Chuan He; Thomas C. Corke; Mehul P. Patel
Flow Measurements in a Short Takeoff, Vertical Landing Fountain: Splayed Jets
pages (874-882)
doi: 10.2514/1.38296
    A. J. Saddington; K. Knowles; P. M. Cabrita
Multidisciplinary Optimization Method for Designing Boundary-Layer-Ingesting Inlets
pages (883-894)
doi: 10.2514/1.38755
    David L. Rodriguez
Thermal Buckling and Flutter Behavior of Shape Memory Alloy Hybrid Composite Shells
pages (895-902)
doi: 10.2514/1.38787
    Hesham Hamed Ibrahim; Hong Hee Yoo; Kwan-Soo Lee
Shock Effects on Delta Wing Vortex Breakdown
pages (903-914)
doi: 10.2514/1.38792
    L. A. Schiavetta; O. J. Boelens; S. Crippa; R. M. Cummings; W. Fritz; K. J. Badcock
Self-Adaptive Upwinding for Large Eddy Simulation of Turbulent Flows on Unstructured Elements
pages (915-926)
doi: 10.2514/1.38945
    Nima Tajallipour; Babak Babaee Owlam; Marius Paraschivoiu
Application of a Pendulum Support Test Rig for Aircraft Stability Derivative Estimation
pages (927-934)
doi: 10.2514/1.38916
    A. Gatto
Grid Quality and Resolution Issues from the Drag Prediction Workshop Series
pages (935-950)
doi: 10.2514/1.39201
    Dimitri J. Mavriplis; John C. Vassberg; Edward N. Tinoco; Mori Mani; Olaf P. Brodersen; Bernhard Eisfeld; Richard A. Wahls; Joseph H. Morrison; Tom Zickuhr; David Levy; Mitsuhiro Murayama
Sizing and Performance-Prediction Method for Rotary-Wing Ejector Nozzles
pages (951-961)
doi: 10.2514/1.39423
    Alex M. Moodie; Daniel P. Schrage; Lakshmi N. Sankar; Mark H. Waters
Drag Characteristics for Optimally Span-Loaded Planar, Wingletted, and C Wings
pages (962-971)
doi: 10.2514/1.39426
    Joram G. Verstraeten; Ronald Slingerland
Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation
pages (972-980)
doi: 10.2514/1.39626
    M. Ghoreyshi; K. J. Badcock; M. A. Woodgate
Influence of Layer Thickness on the Design of Rapid-Prototyped Models
pages (981-987)
doi: 10.2514/1.39702
    C. Aghanajafi; S. Daneshmand; A. Ahmadi Nadooshan
Experimental Investigation of Annular Wing Aerodynamics
pages (988-996)
doi: 10.2514/1.39822
    Lance W. Traub
Aerodynamics of Battle-Damaged Finite-Aspect-Ratio Wings
pages (997-1004)
doi: 10.2514/1.39839
    Peter M. Render; Mujahid Samaad-Suhaeb; Zhiyin Yang; Mahmoud Mani
Magnitude of Corona Current Caused by Aircraft Net Charge
pages (1005-1008)
doi: 10.2514/1.39857
    Xingya Da; Huairong Shen; Lei Hong
Assessment of Passive Flow Control for Transonic Cavity Flow Using Detached-Eddy Simulation
pages (1009-1029)
doi: 10.2514/1.39894
    S. J. Lawson; G. N. Barakos
Potential Panel and Time-Marching Free-Wake-Coupling Analysis for Helicopter Rotor
pages (1030-1041)
doi: 10.2514/1.40001
    Seong Yong Wie; Seongkyu Lee; Duck Joo Lee
In-Flight Estimation of Helicopter Gross Weight and Mass Center Location
pages (1042-1049)
doi: 10.2514/1.41018
    Michael Abraham; Mark Costello
Design of an Electric Propulsion System for a Quadrotor Unmanned Aerial Vehicle
pages (1050-1058)
doi: 10.2514/1.38409
    Michael J. Stepaniak; Frank Van Graas; Maarten Uijt De Haag
Flowfield of a Forward-Facing Shaped-Charge Cavity
pages (1059-1062)
doi: 10.2514/1.38125
    R. Rifki; A. Ahmed
Assessment of Uncertain External Store Aerodynamics Using mu-p Flutter Analysis
pages (1062-1068)
doi: 10.2514/1.39158
    Sebastian Heinze; Ulf Ringertz; Dan Borglund
Flutter Equation as a Piecewise Quadratic Eigenvalue Problem
pages (1068-1070)
doi: 10.2514/1.40653
    David Eller
Multipoint Optimization of a Short-Range Quiet Passenger Aircraft
pages (1070-1074)
doi: 10.2514/1.40726
    Masaya Sunago; Daisuke Sasaki; Keizo Takenaka; Kazuhiro Nakahashi
Noninvasive Measurement of Velocity, Pressure, and Temperature in Unseeded Supersonic Air Vortices
pages (1074-1076)
doi: 10.2514/1.42004
    G. C. Herring
Unsteady Airfoil with Dynamic Leading- and Trailing-Edge Flaps
pages (1076-1081)
doi: 10.2514/1.42431
    T. Lee; P. Gerontakos
Simple Quantitative Method to Compare Aircraft Wing Mode Shapes
pages (1082-1084)
doi: 10.2514/1.42777
    Charles M. Denegri
Effects of Gurney Flaps on an Annular Wing
pages (1085-1088)
doi: 10.2514/1.43096
    Lance W. Traub
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