Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6
Author:
Affiliation:
1. Vikram Sharabhai Space Center, Trivandrum 695 022, India
2. Nanyang Technological University, Singapore 639 798, Republic of Singapore
3. Indian Institute of Technology, Kanpur 208 016, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.46023
Reference13 articles.
1. Unsteady Aerodynamic Considerations in the Design of a Drag-Reduction Spike
2. Transonic flow modes of an axisymmetric blunt body
3. Chang, P. K., Separation of Flow, Pergamon, New York, 1970, pp.469-530.
4. Modes of shock-wave oscillations on spike-tipped bodies
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