An official website of the United States Government
An official website of the United States Government
| Add to Bookshelf | | |
| Choose format: | Standard | | | Short | | | MARC |
| Title | Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. II, Mass distributed along the fuselage / |
| Format | online resource |
| Internet Access | https://purl.fdlp.gov/GPO/gpo158487 |
| Author |
 Seidman, Oscar, author.
|
| Published | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937. |
|
|
|
| SuDoc Number |
Y 3.N 21/5:6/630
|
| Variation of Title |
Mass distributed along the fuselage
|
| Description | 1 online resource (11 pages, 17 unnumbered pages) : illustrations. |
| Content Type | text |
| Series |
(Technical note (United States. National Advisory Committee for Aeronautics) ; 630.)
|
| General Note | "December 1937." |
| No Federal Depository Library Program (FDLP) item number. | |
| Bibliography | Includes bibliographical references (page 11). |
| Metadata Source | Description based on online resource, PDF version; title from title page (TRAIL, viewed August 4, 2021). |
| Subject - LC |
Spin (Aerodynamics)
|
|
Airplanes -- Fuselage.
|
|
|
Airplanes -- Tail surfaces.
|
|
|
Airplanes -- Wings.
|
|
|
Mass (Physics)
|
|
|
Wind tunnel testing.
|
|
|
Aerodynamic load.
|
|
| Added Entry |
Neihouse, A. I., author.
|
| Added Entry |
United States. National Advisory Committee for Aeronautics, issuing body.
|
| Linking Field |
Print version: Seidman, Oscar Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. 2. Mass distributed along the fuselage (OCoLC)645506267
|
| URL | Address at time of PURL creation https://digital.library.unt.edu/ark:/67531/metadc54437/m2/1/high_res_d/19930081451.pdf |
|
|
|
| Holdings | All items |
|
|
|
| OCLC Number | (OCoLC)1159597641 |
| CGP Record Link | https://catalog.gpo.gov:443/F/?func=direct&doc_number=001162979&local_base=GPO01PUB |
| System Number | 001162979 |
