Effect of mass injection on the drag of a slender cone in hypersonic flow-Reference-Cited by-同舟云学术

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Effect of mass injection on the drag of a slender cone in hypersonic flow

Published:1964-05 Issue:5 Volume:2 Page:836-844
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

KING HARTLEY H.¹,TALBOT LAWRENCE¹

Affiliation:

1. University of California, Berkeley, Calif

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2439

Reference20 articles.

1. Talbot, L , "Viscosity corrections to cone probes in rarefied supersonic flow at a nominal Mach number of 4," NACA TN 3219(1954)

2. Maslach, G J and Talbot, L , "Low density aerodynamic characteristics for a cone at angle of attack," Univ of California Engineering Project Rept HE-150-172 (1959)

Cited by 14 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. Ballistic range tests of ablating and nonablating slender cones;AIAA Journal;1970-03

2. A pressure-interaction theory for axisymmetric, hypersonic, laminar,unseparated flows;8th Aerospace Sciences Meeting;1970-01-19

3. Unsteady laminar boundary layers on an infinite plate in an optically thick radiating gas;Applied Scientific Research;1970-01

4. Effect of gaseous injection on the hypersonic flow around transpiration-cooled bodies.;Journal of Spacecraft and Rockets;1969-06

5. Binary boundary layers on sharp cones in low-density supersonic and hypersonic flow.;AIAA Journal;1969-04

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