E-book
Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. II. Mass distributed along the fuselage / by Oscar Seidman and A.I. Neihouse.
Record details
- Physical Description: 1 online resource (11 pages, 17 unnumbered pages) : illustrations.
- Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1937.
Content descriptions
| General Note: | "December 1937." No Federal Depository Library Program (FDLP) item number. |
| Bibliography, etc. Note: | Includes bibliographical references (page 11). |
| Source of Description Note: | Description based on online resource, PDF version; title from title page (TRAIL, viewed August 4, 2021). |
Search for related items by subject
| Subject: | Spin (Aerodynamics) Airplanes > Fuselage. Airplanes > Tail surfaces. Airplanes > Wings. Mass (Physics) Wind tunnel testing. Aerodynamic load. |
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| LDR | 02328nam a2200469 i 4500 | ||
|---|---|---|---|
| 001 | on1159597641 | ||
| 003 | OCoLC | ||
| 005 | 20210825104918.0 | ||
| 006 | m o d f | ||
| 007 | cr b|||||||||| | ||
| 008 | 200623s1937 dcua gob f000 0 eng c | ||
| 042 | . | ‡apcc | |
| 040 | . | ‡aTRAAL ‡beng ‡erda ‡epn ‡cTRAAL ‡dOCLCO ‡dOCLCF ‡dGPO ‡dMvI | |
| 074 | . | ‡a9999 (online) | |
| 086 | 0 | . | ‡aY 3.N 21/5:6/630 |
| 100 | 1 | . | ‡aSeidman, Oscar, ‡eauthor. |
| 245 | 1 | 0. | ‡aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. ‡nII. ‡pMass distributed along the fuselage / ‡cby Oscar Seidman and A.I. Neihouse. |
| 246 | 3 | 0. | ‡aMass distributed along the fuselage |
| 264 | 1. | ‡aWashington, [D.C.] : ‡bNational Advisory Committee for Aeronautics, ‡c1937. | |
| 300 | . | ‡a1 online resource (11 pages, 17 unnumbered pages) : ‡billustrations. | |
| 336 | . | ‡atext ‡btxt ‡2rdacontent | |
| 337 | . | ‡acomputer ‡bc ‡2rdamedia | |
| 338 | . | ‡aonline resource ‡bcr ‡2rdacarrier | |
| 490 | 1 | . | ‡aTechnical note / National Advisory Committee for Aeronautics ; ‡vNo. 630 |
| 588 | . | ‡aDescription based on online resource, PDF version; title from title page (TRAIL, viewed August 4, 2021). | |
| 500 | . | ‡a"December 1937." | |
| 500 | . | ‡aNo Federal Depository Library Program (FDLP) item number. | |
| 504 | . | ‡aIncludes bibliographical references (page 11). | |
| 650 | 0. | ‡aSpin (Aerodynamics) ‡0(EG-IN)645673 | |
| 650 | 0. | ‡aAirplanes ‡xFuselage. ‡0(EG-IN)1255087 | |
| 650 | 0. | ‡aAirplanes ‡xTail surfaces. ‡0(EG-IN)1255324 | |
| 650 | 0. | ‡aAirplanes ‡xWings. ‡0(EG-IN)1255373 | |
| 650 | 0. | ‡aMass (Physics) ‡0(EG-IN)572533 | |
| 650 | 0. | ‡aWind tunnel testing. ‡0(EG-IN)1018265 | |
| 650 | 0. | ‡aAerodynamic load. ‡0(EG-IN)1251803 | |
| 700 | 1 | . | ‡aNeihouse, A. I., ‡eauthor. ‡0(DLC)1585178 |
| 710 | 1 | . | ‡aUnited States. ‡bNational Advisory Committee for Aeronautics, ‡eissuing body. ‡0(EG-IN)1039303 |
| 776 | 0 | 8. | ‡iPrint version: ‡aSeidman, Oscar ‡tFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. 2. Mass distributed along the fuselage ‡w(OCoLC)645506267 |
| 830 | 0. | ‡aTechnical note (United States. National Advisory Committee for Aeronautics) ; ‡v630. ‡0(EG-IN)1504386 | |
| 856 | 4 | 0. | ‡uhttps://purl.fdlp.gov/GPO/gpo158487 ‡9STLIB-IND |
| 949 | . | ‡hONLINE | |
| 901 | . | ‡aon1159597641 ‡bOCoLC ‡c22200375 ‡tbiblio ‡sGPO - Government Documents | |
