Diagnostic Investigation of Fluid Flow Characteristics of Aerospike Nozzles During Streamtube Compression and Shock Wave Generation at Various Pressure Ratios
Author:
Affiliation:
1. Amity University
2. Vikram Sarabhai Space Centre
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-4446
Reference59 articles.
1. V.R.Sanal Kumar et al. "The theoretical prediction of the boundary layer blockage and external flow choking at moving aircraft in ground effects," Phys Fluids 33(2021),
2. Performance Characteristics of an Annular Conical Aerospike Nozzle with Freestream Effect
3. Study of Conical Aerospike Nozzles with Base-Bleed and Freestream Effects
4. Computational study of performance characteristics for truncated conical aerospike nozzles
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