An optimization procedure for the design of prop-rotors in high speed cruise including the coupling of performance, aeroelastic stability, and structures-Reference-Cited by-同舟云学术

An optimization procedure for the design of prop-rotors in high speed cruise including the coupling of performance, aeroelastic stability, and structures

Published:1994-02 Issue:3-4 Volume:19 Page:75-88
ISSN:0895-7177
Container-title:Mathematical and Computer Modelling
language:en
Short-container-title:Mathematical and Computer Modelling

Author:

Chattopadhyay A.,McCarthy T.R.,Madden J.F.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference24 articles.

1. Selected design issues of some high speed rotorcraft concepts;Talbot;AIAA/AHS/ASEE Aircraft Design, Systems and Operations Conference,1990

2. Technology needs for high speed rotorcraft (1);Wilkerson;NASA CR 177585,1991

3. Technology needs for high speed rotorcraft (2);Scott;NASA CR 177590,1991

4. Technology needs for high speed rotorcraft;Rutherford;NASA CR 177578,1991

5. Parametric studies for tilt-rotor aeroelastic stability in high-speed flight;Nixon;AIAA Paper No. 92-2568,1992

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1. Analytic extraction of the elastic coupling mechanisms in composite blades;Composite Structures;2000-08

2. Recent Applications of Design Optimization to Rotorcraft-A Survey;Journal of Aircraft;1999-01

3. A Coupled Rotor/Wing Optimization Procedure for High Speed Tilt-Rotor Aircraft;Journal of the American Helicopter Society;1996-10-01

4. A Performance Based Optimization of High Speed Prop‐Rotors;Journal of the American Helicopter Society;1995-07-01

5. Multilevel decomposition procedure for efficient design optimization of helicopter rotor blades;AIAA Journal;1995-02