Subsonic diffuser design and performance for advanced fighter aircraft-Reference-Cited by-同舟云学术

Subsonic diffuser design and performance for advanced fighter aircraft

Published:1985-08-17 Issue: Volume: Page:
ISSN:
Container-title:Aircraft Design Systems and Operations Meeting
language:
Short-container-title:

Author:

LEE C.¹,BOEDICKER C.²

Affiliation:

1. McDonnell Aircraft Co., St. Louis, MO

2. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-3073

Reference11 articles.

1. Kitchen. R . A. and Sedlock. D. "Subsonic Diffuser Development For Advanced Tactical Aircraft", AIAA 83-1168.

2. Neumann, H. E., Povinell, L. A., and Coltrin, I(. E. "An Analytical and Experimental Study of a Short S-Shaped Subsonic Uiffusers of a Supersonic Inlet", AIAA 80-0386.

3. Slair, L. W. and RUSSO, C. J . "Compact Diffusers for Centrifugal Compressions", AIM-80-1077.

4. Little, B. H. Jr. and Trimboli, "An Experimental Investigation of S-Duct Diffusers for High-speed Prop-Fans", AIAA-82-1123.

5. Povinelli, L. A. "Am Experimental and Analytical Investigation of .Axisymetric Diffusers", AIAA Paper 75-1211.

Cited by 40 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multi-Objective Bayesian Optimization Design of Elliptical Double Serpentine Nozzle;Aerospace;2023-12-31

2. Thermal–Solid Interaction Study of Serpentine Nozzle and Analysis on Structural Response Law;Journal of Applied Fluid Mechanics;2023-12-01

3. An integrated topology and shape optimization framework for stiffened curved shells by mesh deformation;Engineering with Computers;2023-09-22

4. Multi-objective shape optimization of doubly offset serpentine diffuser using Adjoint method;International Journal of Heat and Fluid Flow;2023-08

5. Study on the Influence of Vortex Generator on Aerodynamic and Stealth Characteristics of Serpentine Inlet;AIAA AVIATION 2023 Forum;2023-06-08