ScholarLens Back to search
1967•NASA Technical Reports Server (NASA)Requires access

Two approximate solutions of the hypersonic blunt-body problem.

A. C. Gudikunst, E. K. Huckins

Open publisher page 0 citations

Abstract

Axisymmetric blunt bodies shock standoff distances in hypersonic flow determined by numerical and analytic methods

About this research paper

What this paper is about

Axisymmetric blunt bodies shock standoff distances in hypersonic flow determined by numerical and analytic methods

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Axisymmetric blunt bodies shock standoff distances in hypersonic flow determined by numerical and analytic methods

Key concepts: Blunt, Mathematics, Computer science, Medicine, Surgery

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Two approximate solutions of the hypersonic blunt-body problem. — Research Paper | ScholarLens