Research Catalog

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

Title
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.
Author
Driver, Cornelius
Publication
Washington : National Aeronautics and Space Administration, September 1959.

Available Online

0

Details

Additional Authors
United States. National Aeronautics and Space Administration, issuing body.
Description
1 online resource (47 pages) : illustrations.
Series Statement
NASA/TM ; X-116
Uniform Title
NASA technical memorandum ; X-116.
Subject
  • Hypersonic aircraft
  • Aerodynamic characteristics
  • Aerodynamics
  • Aerodynamic measurements
  • Mach number
  • Hypersonic planes
  • Wind tunnel testing
  • Shells (Engineering)
  • Noses (Aircraft)
Note
  • "September 1959"--Cover.
Bibliography (note)
  • Includes bibliographical references (page 6).
Type of Report (note)
  • Technical memorandum.
Source of Description (note)
  • Description based on online resource; title from PDF cover, (NASA, viewed on May 26, 2022).
Call Number
GPO Internet NAS 1.15:X-116
OCLC
marcive761192031
Author
Driver, Cornelius, author.
Title
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
Washington : National Aeronautics and Space Administration, September 1959.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; X-116
NASA technical memorandum ; X-116.
Bibliography
Includes bibliographical references (page 6).
Type Of Report
Technical memorandum.
Connect to:
https://purl.fdlp.gov/GPO/gpo182854
Added Author
United States. National Aeronautics and Space Administration, issuing body.
Other Form:
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.
0830-D (online)
Sudoc No.
NAS 1.15:X-116
View in Legacy Catalog