Cross Section Controllable Hypersonic Inlet Design Using Streamline-Tracing and Osculating Axisymmetric Concepts

Author(s):

• Y. You ( Nanjing University of Aeronautics and Astronautics, Nanjing, China (prc) )
• D. Liang
• G. Huang

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-5379

Paper no.:

AIAA Paper 2007-5379

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200716 [CD-ROM 2007 Disc 16]

Type:

Technical Paper