Title

Source Flow Effects In Conical Hypervelocity Nozzles

Date

1962

Index Abstract

Coming Soon

Photo Quality

Complete

Report Number

AEDC TDR 62-116

Creator

Whitfield, Jack D.

Norfleet, Glenn D.

Corporate Author

Arnold Engineering Development Center Arnold Air Force Station Tenn

Laboratory

Arnold Engineering Development Center

Extent

20

Identifier

AD0276724

Access Rights

ASTIA

Distribution Classification

1

Contract

AF 40(600)-800

DoD Project

8952

DoD Task

895202

DTIC Record Exists

No

Distribution Change Authority Correspondence

None

Abstract

Source flow effects in conical hypervelocity nozzles are studied by means of a simple Newtonian theory for slender conical bodies. Experiments were conducted to examine the validity of this simple theoretical approach and a semiempirical theory is developed to assess the magnitude of source flow effects. Significant source flow effects were found, and the need for contoured hypervelocity wind tunnel nozzles is shown.

Report Availability

Full text available

Date Issued

1962-06

Publisher

Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force

Provenance

IIT

Type

report

Format

1 online resource