Journal ArticleDOI
Integrated design of fighters with stores for best airforce value
TLDR
In this paper, the development of fighters integrated with their stores is reviewed, with the main aerodynamic effects of stores being higher drag (store much reducing operational area), store trajectory disturbed at release (missing target or even colliding with aircraft), and reduced performance and agility of loaded aircraft.About:
This article is published in Progress in Aerospace Sciences.The article was published on 1998-04-14. It has received 4 citations till now.read more
Citations
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Journal ArticleDOI
Mixed design of radar/infrared stealth for advanced fighter intake and exhaust system
Zeyang Zhou,Jun Huang +1 more
TL;DR: MDA is effective and efficient in terms of radar/infrared integrated stealth design for the intake and exhaust systems of advanced fighters.
Journal ArticleDOI
Acoustic and radar integrated stealth design for ducted tail rotor based on comprehensive optimization method
Zeyang Zhou,Jun Huang,Nana Wu +2 more
TL;DR: The proposed approach is very effective and efficient for the acoustic/radar comprehensive stealth design of the ducted tail rotor and generated by comprehensive optimization method based on Pareto solution.
Journal ArticleDOI
Grid transformation and dynamic scattering for tail rotor radar cross section analysis
Zeyang Zhou,Jun Huang +1 more
TL;DR: The research on the dynamic radar cross section (RCSRCS) of a helicopter rotor is becoming more and more importan... as mentioned in this paper, with the promotion and enhancement of stealth technology of helicopter rotor components.
Proceedings ArticleDOI
Affordable hybrid simulation for predicting store separation
Jaakko Hoffren,Esa Salminen +1 more
References
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Proceedings ArticleDOI
A 3-D Chimera Grid Embedding Technique
TL;DR: A three-dimensional (3-D) chimera grid-embedding technique that simplifies the construction of computational grids about complex geometries by solution of the Euler equations for the transonic flow about a wing/body, wing/ body/tail, and a configuration of three ellipsoidal bodies is described.
Chimera. A Grid-Embedding Technique
TL;DR: The technique simplifies the construction of computational grids about complex geometries by solution of the Euler equations for transonic flow about three ellipsoid bodies in close proximity, aWing/body, and a wing/body/tail.
Journal ArticleDOI
Cruise performance and range prediction reconsidered
TL;DR: In this paper, a unified analytical treatment of the cruise performance of subsonic transport aircraft is derived, valid for gas turbine powerplant installations: turboprop, turbojet and turbofan powered aircraft.
A Preliminary Method for Calculating the Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack Including Effects of Roll Angle and Control Deflections
TL;DR: In this paper, a method is presented together with a computer program for calculating the forces and moments on the components of a cruciform missile: nose, canard section, afterbody, and tail section.
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