Volume 41; Issue 5

Journal of Aircraft

Volume 41; Issue 5
1

Uncertainty Quantification in Aeroelasticity: Recent Results and Research Challenges

Year:
2004
Language:
english
File:
PDF, 1.42 MB
english, 2004
4

Probabilistic Two-Phase Aircraft Wake Vortex Model: Application and Assessment

Year:
2004
Language:
english
File:
PDF, 1.42 MB
english, 2004
5

Numerical Study of Blowing and Suction Control Mechanism on NACA0012 Airfoil

Year:
2004
Language:
english
File:
PDF, 903 KB
english, 2004
6

The mu-k Method for Robust Flutter Solutions

Year:
2004
Language:
english
File:
PDF, 1.02 MB
english, 2004
7

Numerical and Experimental Study of Flow Structure of Low-Aspect-Ratio Wing

Year:
2004
Language:
english
File:
PDF, 5.57 MB
english, 2004
8

High Speed Flight Vehicle Structures: An Overview

Year:
2004
Language:
english
File:
PDF, 2.82 MB
english, 2004
9

Transition on a High-Lift Swept Wing in the European Project EUROLIFT

Year:
2004
Language:
english
File:
PDF, 1.49 MB
english, 2004
10

Interdependence of Diffusion and Straining of Helicopter Blade Tip Vortices

Year:
2004
Language:
english
File:
PDF, 1.45 MB
english, 2004
11

Structure and Induced Drag of a Tip Vortex

Year:
2004
Language:
english
File:
PDF, 5.45 MB
english, 2004
12

Nonlinear Flutter Aspects of the Flexible HIgh-Speed Civil Transport Semispan Model

Year:
2004
Language:
english
File:
PDF, 446 KB
english, 2004
14

Method for Steerable Clustered Round Parachutes

Year:
2004
Language:
english
File:
PDF, 2.01 MB
english, 2004
17

Dynamic Stall Control Based on an Optimal Approach

Year:
2004
Language:
english
File:
PDF, 2.67 MB
english, 2004
18

Preliminary Design of a Structural Wing Box Under a Twist Constraint Part I

Year:
2004
Language:
english
File:
PDF, 2.23 MB
english, 2004
19

Edge Vortices of a Double Element Wing in Ground Effect

Year:
2004
Language:
english
File:
PDF, 3.58 MB
english, 2004
20

First Look into Effects of Discrete Midspan Vortex Injection on Wing Performance

Year:
2004
Language:
english
File:
PDF, 2.26 MB
english, 2004
21

Transient Helicopter Rotor Wakes in Response to Time-Dependent Blade Pitch Inputs

Year:
2004
Language:
english
File:
PDF, 5.75 MB
english, 2004
23

History of Flight Vehicle Structures 1903-1990

Year:
2004
Language:
english
File:
PDF, 2.98 MB
english, 2004
24

Lifting-Line Analysis of Roll Control and Variable Twist

Year:
2004
Language:
english
File:
PDF, 1.17 MB
english, 2004
26

Application of Vortex Invariants to Roll Up of Vortex Pairs

Year:
2004
Language:
english
File:
PDF, 256 KB
english, 2004
27

Effects of Synthetic Jet Actuation on a Ramping NACA 0015 Airfoil

Year:
2004
Language:
english
File:
PDF, 3.60 MB
english, 2004
28

Forced Response of a Vortex Filament Pair Measured in a Water Tunnel

Year:
2004
Language:
english
File:
PDF, 1.26 MB
english, 2004
29

Visualized Vortices on Unmanned Combat Air Vehicle Planform: Effect of Reynolds Number

Year:
2004
Language:
english
File:
PDF, 2.06 MB
english, 2004
30

Near-Wake Characteristics of an Oscillating NACA 4412 Airfoil

Year:
2004
Language:
english
File:
PDF, 406 KB
english, 2004