Advanced method for computing the flow around wings with rear separation and ground effect /
में बचाया:
| OCLC: | 20474918 |
|---|---|
| मुख्य लेखक: | |
| भाषा: | English |
| प्रकाशित: |
Köln :
DFVLR,
1986.
|
| श्रृंखला: | Forschungsbericht (Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt) ;
86-17. |
| विषय: | |
| Global Resources Program: | Southeast Asia Materials Project (SEAM) |
| स्वरूप: | Monograph Note that CRL will digitize material from the collection when copyright allows. |
| LEADER | 01713cam a2200397Ma 4500 | ||
|---|---|---|---|
| 001 | in00005445553 | ||
| 003 | OCoLC | ||
| 008 | 870707s1986 gw a b 000 0 eng d | ||
| 005 | 20240531184450.5 | ||
| 035 | |a (OCoLC)20474918 | ||
| 040 | |a UBY |c UBY |d CRL | ||
| 041 | 0 | |a eng |b ger | |
| 049 | |a CRLM | ||
| 099 | |a C-29805 | ||
| 100 | 1 | |a Jacob, K. |q (Klaus), |d 1936- | |
| 245 | 1 | 0 | |a Advanced method for computing the flow around wings with rear separation and ground effect / |c Klaus Jacob. |
| 260 | |a Köln : |b DFVLR, |c 1986. | ||
| 300 | |a 62 p. : |b ill. ; |c 23 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a DFVLR-FB, |x 0171-1342 ; |v 86-17. | |
| 500 | |a At head of title: DFVLR. Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt. | ||
| 500 | |a "Forschungsbericht." | ||
| 500 | |a Summary in German. | ||
| 504 | |a Includes bibliographical references (p. 39-41) | ||
| 650 | 0 | |a Aerodynamics. | |
| 650 | 0 | |a Airplanes |x Wings. | |
| 650 | 0 | |a Ground-cushion phenomenon. | |
| 830 | 0 | |a Forschungsbericht (Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt) ; |v 86-17. | |
| 907 | |a .b13654366 |b 05-31-24 |c 09-10-93 | ||
| 990 | |m CRL | ||
| 998 | |a crlm |b 09-15-93 |c m |d - |e - |f eng |g gw |h 0 |i 1 | ||
| 999 | f | f | |i b32bb600-4d1d-5786-9711-df1a59b8e745 |s 25d0d68c-bb44-5766-8cf0-85464d7d0efe |t 0 |