Research Catalog

Details

Additional authors

1. United States. National Aeronautics and Space Administration, issuing body.

Description

1. 1 online resource (47 pages) : illustrations.

Series statement

1. NASA/TM ; X-116

Uniform title

1. NASA technical memorandum ; X-116.

Subject

1. Hypersonic aircraft
2. Aerodynamic characteristics
3. Aerodynamics
4. Aerodynamic measurements
5. Mach number
6. Hypersonic planes
7. Wind tunnel testing
8. Shells (Engineering)
9. Noses (Aircraft)

Call number

1. GPO Internet NAS 1.15:X-116

Note

1. "September 1959"--Cover.

Bibliography (note)

1. Includes bibliographical references (page 6).

Type of report (note)

1. Technical memorandum.

Source of description (note)

1. Description based on online resource; title from PDF cover, (NASA, viewed on May 26, 2022).

Author

1. Driver, Cornelius, author.

Title

1. Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.

Publisher

1. Washington : National Aeronautics and Space Administration, September 1959.

Type of content

1. text

Type of medium

1. computer

Type of carrier

1. online resource

Series

1. NASA/TM ; X-116
2. NASA technical memorandum ; X-116.

Bibliography

1. Includes bibliographical references (page 6).

Type of report

1. Technical memorandum.

Connect to:

1. https://purl.fdlp.gov/GPO/gpo182854

Added author

1. United States. National Aeronautics and Space Administration, issuing body.

Other form:

1. Print version: Driver, Cornelius Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 (OCoLC)688628077

Gpo item no.

1. 0830-D (online)

Sudoc no.

1. NAS 1.15:X-116