Conical nose shape effects on drag and static stability at Mach 10.
Author:
Affiliation:
1. General Electric Company, Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.30384
Reference6 articles.
1. Aerothermodynamic characteristics of slender ablating re-entry vehicles
2. Test Facilities Handbook, Eighth Edition, Vol. 4, Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, Tullahoma, Tenn. Dec., 1969, pp.5.1-5.12.
Cited by 4 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. Ablative nose shape change effects on re-entry vehicle aerodynamic performance;2nd Atmospheric Flight Mechanics Conference;1972-08-16
2. Effect of Polarization on the Apparent Emittance of Rectangular Groove Cavities;AIAA Journal;1972-08
3. Prediction of Nose Shape Effects on Nonlinear Stability Characteristics of Slender Cones;AIAA Journal;1972-08
4. Effect on Slender Vehicle Dynamics of Change from Spherical to Conical Nose Bluntness;Journal of Spacecraft and Rockets;1972-06
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