Research Catalog

Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model

Title
Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / Aparajit J. Mahajan [and three others].
Author
Mahajan, Aparajit J.
Publication
Washington, D.C. : NASA, April 1992.

Available Online

0

Details

Additional Authors
United States. National Aeronautics and Space Administration, issuing body.
Description
1 online resource (approximately 14 pages) : illustrations.
Series Statement
NASA/TM ; 105268
Uniform Title
NASA technical memorandum ; 105268.
Subject
  • Prop-fan technology
  • Flutter
  • Cruise missiles
Note
  • "April 1992."
Bibliography (note)
  • Includes bibliographical references (pages 6-7).
Type of Report (note)
  • Technical memorandum.
Source of Description (note)
  • Description based on online resource, PDF version; title from title page (NASA, viewed on Jan. 6, 2022).
Call Number
GPO Internet NAS 1.15:105268
OCLC
marcive1291212594
Author
Mahajan, Aparajit J., author.
Title
Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / Aparajit J. Mahajan [and three others].
Publisher
Washington, D.C. : NASA, April 1992.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 105268
NASA technical memorandum ; 105268.
Bibliography
Includes bibliographical references (pages 6-7).
Type Of Report
Technical memorandum.
Connect to:
https://purl.fdlp.gov/GPO/gpo173618
Added Author
United States. National Aeronautics and Space Administration, issuing body.
Other Form:
Microfiche version: Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model (OCoLC)27007869
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:105268
View in Legacy Catalog