Email RIS file
Bookmark
Report an Issue

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at Mach 1.60, 2.36, and 3.70. Volume 3 : Cranked tail

Author:
Sawyer, W. C.
Published:
Aug 1, 1979.
Physical Description:
1 electronic document
Additional Creators:
Babb, C. D., Wassum, D. L., and Lamb, M.
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access:
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
The results of pressure distribution tests are presented without analysis. The test Reynolds number used was 6.6. x 10 to the 6th power per meter.
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19790019969.
Accession ID: 79N28140.
NASA-TM-80097-VOL-3.
L-12993-VOL-3.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15725004