ScholarLens Back to search
1968•NASA Technical Reports Server (NASA)Open access

Wind-tunnel calibration of a 40 deg conical pressure probe at Mach numbers from 3.5 to 7.4

Frank W. Burcham

Open full text 1 citations

Abstract

Wind tunnel calibration of conical pressure probe over range of Mach numbers to determine flow field data for X-15 airplane

Open-access reader

About this research paper

What this paper is about

Wind tunnel calibration of conical pressure probe over range of Mach numbers to determine flow field data for X-15 airplane

Why it matters

OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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

Wind tunnel calibration of conical pressure probe over range of Mach numbers to determine flow field data for X-15 airplane

Key concepts: Calibration, Mach number, Wind tunnel, Supersonic wind tunnel, Conical surface, Static pressure, Physics, Mechanics

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Wind-tunnel calibration of a 40 deg conical pressure probe at Mach numbers from 3.5 to 7.4 — Research Paper | ScholarLens