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Results 1-10 of 10 (Search time: 0.003 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence Models

Choi S.W.; Chang, Keun Sick; Ok Honam, JOURNAL OF AIRCRAFT, v.38, no.5, pp.888 - 894, 2001-09

2
Navier-Stokes Computation of A Rapidly Deploying Spoiler

Choi S.W.; Chang, Keun Sick, JOURNAL OF AIRCRAFT, v.37, no.4, pp.655 - 661, 2000-07

3
Effect of external acoustic excitation on NACA0015 discrete tonal noise

Andan, Amelda D.; Lee, Duck-Joo, APPLIED ACOUSTICS, v.141, pp.374 - 381, 2018-12

4
Generalized transonic unsteady aerodynamics via computational-fluid-dynamics/indicial approach

Marzocca, P; Librescu, L; Kim, DH; Lee, In; Schober, S, AIAA JOURNAL, v.43, no.4, pp.915 - 917, 2005-04

5
Frequency and time domain flutter computations of a wing with oscillating control surface including shock interference effects

Kwon, HJ; Kim, DH; Lee, In, AEROSPACE SCIENCE AND TECHNOLOGY, v.8, no.6, pp.519 - 532, 2004-09

6
Nonlinear aeroelastic analysis of a deployable missile control fin

Bae, Jae-Sung; Kim, Dae-Kwan; Shin, Won-Ho; Lee, In; Kim, Seung-Ho, JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.2, pp.264 - 271, 2004-03

7
Nonlinear aeroelastic analysis for a control fin with an actuator

Shin, WH; Lee, In; Shin, YS; Bae, JS, JOURNAL OF AIRCRAFT, v.44, no.2, pp.597 - 605, 2007-03

8
Nonlinear aeroelastic analysis of control with freeplay in transonic region

Park, YK; Yoo, JH; Lee, In, AIAA JOURNAL, v.45, no.5, pp.1142 - 1145, 2007-05

9
Effects of actuator nonlinearity on aeroelastic characteristics of a control fin

Shin, WH; Lee, SJ; Lee, In; Bae, JS, JOURNAL OF FLUIDS AND STRUCTURES, v.23, no.7, pp.1093 - 1105, 2007-10

10
Development of an indicial function approach for the two-dimensional incompressible/compressible aerodynamic load modelling

Marzocca, P; Librescu, L; Kim, DH; Lee, In; Schober, S, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.221, pp.453 - 463, 2007-06

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