Theoretical studies on the effects of blowing and suction in laminarseparated regions

Author:

STRAHLE W.1

Affiliation:

1. AEROSPACE CORP., SAN BERNARDINO, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. I. Kehlet, A. B. "Free flight investigation of comparative zero-lift rolling effectiveness of a leading-edge and a trailing-edge air-jet spoiler on an unswept wing," NACA RM L57F10 (August 1957) Strike, W. T., Schueler, C. J., and Deitering, J. S. "Interactions produced by sonic lateral jets located on surfaces in a supersonic stream,I' AEDC TDR63-22 (April 1963) Kallis, J. M. and Adelberg, M. "Recent advances in the fluid dynamics of gas injection for thrust-vector and trajectory cantrol, Aerospace Corporation Report No. ATN-63(3305)-3 (15 July 1963)

2. Lees, L. and Reeves, B. L. "Supersonic separated and reattaching laminar flows: I. General theory and application to adiabatic boundary layer layerishock wave interactions, I' AIAA J. 2, 1907 - 1920 (1964)

3. Abbott, D. E., Holt, M., and Nielsen, J. N. "Studies of separated laminar boundary layers at hypersonic speed with Some low Reynolds number data, AIAA Paper 63-172 (June 17-20, 1963)

4. NASA Tech. Note D-1072 (September 1961)

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3