Access provided by Rice University
Sign in
|
Register
|
Mobile
|
Cart
Home
Browse
About Multi-Science
Subscriptions
Multi-Science Agents
Author Instructions
Sample Copies
Contact Us
Search in:
This Journal
Anywhere
Advanced search
Home
>
International Journal of Aerospace Innovations
>
List of Issues
>
Volume 4, Issue 1-2
International Journal of Aerospace Innovations
Print ISSN:
1757-2258
Ahead of print
Current issue
List of issues
About this journal
Authors and Submissions
Get TOC alerts
Subscribe
< Previous issue
Next issue >
Volume 4, Issue 1-2, March 2012
Select All
For selected items:
Please select
Add to Favorites
Track Citation
Download Citation
Email
Research Article
Preface
4(1-2)
,
pp. i–ii
Citation
|
PDF (56 KB)
Three-Dimensional Density Measurement of Supersonic and Axisymmetric Flow Field by Colored Grid Background Oriented Schlieren (CGBOS) Technique
Masanori Ota
,
Hiroko Kato
,
Kazuo Maeno
4(1-2)
,
pp. 1–12
Abstract
|
References
|
PDF (2474 KB)
Flow Topology and Secondary Separation Modelling at Crossing Shock Wave/Turbulent Boundary Layer Interaction Conditions
Andrea Salin
,
Yufeng Yao
,
Alexander Zheltovodov
4(1-2)
,
pp. 13–28
Abstract
|
References
|
PDF (1476 KB)
Shock-Wave Boundary-Layer Interaction Study on a Compression Corner Using Pressure-Sensitive Paint
C. Manisankar
,
S. Verma
,
C. Raju
4(1-2)
,
pp. 29–40
Abstract
|
References
|
PDF (1222 KB)
On Numerical Techniques for Determination of the Sonic Point in Unsteady Inviscid Shock Reflections
Ali Hakkaki-Fard
,
Evgeny Timofeev
4(1-2)
,
pp. 41–52
Abstract
|
References
|
PDF (761 KB)
Numerical and Experimental Investigations of Fluidic Thrust Vectoring Mechanism
Li Li
,
Tsutomu Saito
4(1-2)
,
pp. 53–64
Abstract
|
References
|
PDF (946 KB)
Most Read
Most Cited
CFD Simulation of Flow Past MAV Wings
Design and Analysis Tool for Mars Atmospheric Entry Missions
CFD Analysis of a Launch Vehicle with Reverse Flow Nozzles-A Validation Study
Supersonic Testing of NAL Binary Pressure Sensitive Paint
Application of System Identification Techniques to Tejas Flight Test Data
See More
Numerical and Experimental Investigations of Fluidic Thrust Vectoring Mechanism
Subscription Options
Individual Offers
International Journal of Aerospace Innovations (2015) (print and online): GBP 308.00
International Journal of Aerospace Innovations (2015) (print only): GBP 299.00
International Journal of Aerospace Innovations (2015) (online only): GBP 278.00