Komm zurück

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle

Schurmeier, H. M.

Information

Sie können es in finden

Kategorie

Testo

Natur

Monografia

Titel

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle

Namen

[Autore] Schurmeier, H. M.
AGARD

Beschreibung

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle / by H. M. Schurmeier

Physische Beschreibung

XIII, 156 p., p. di tav. : ill. ; 27 cm.

Datum

1959

Ort der Veröffentlichung

Paris

Dorf

FRANCIA

Zunge

INGLESE

Quelle

Biblioteche SBN Sardegna

IT\ICCU\RMS\1096810

Ressourcenverbindungen

http://id.sbn.it/bid/RMS1096810

Etikett

Bilder

Master resistivity curves for a two-, three-, and four-layer earth

Autor : Mooney, Harold Morton

Jahr : 1956

"War against terrorism" is the new stage of the continuous war wich is waged with econimic, political and military means ..

Jahr : 2001

Ergebnisse 2 von 83799

Alle ansehen

Texte

A summary of the techniques of variable Mach number supersonic wind tunnel nozzle design

Autor : Kenney, J. T.

Jahr : 1954

Two-dimensional wind tunnel wall interference

Autor : Mokry, M.

Jahr : 1983

Ergebnisse 2 von 2187115

Alle ansehen

Video

Fuori dal tunnel

Jahr : 1991

None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

Jahr : 1990

Ergebnisse 2 von 70636

Alle ansehen

Audio

Two of a mind

Autor : Desmond, Paul

Jahr : 2010

A zed and two noughts : [original music from the film by Peter Greenaway]

Autor : Nyman, Michael

Jahr : 2004

Ergebnisse 2 von 25642

Alle ansehen

Kommentare

Andere laden

Schreibe einen Kommentar

Schicken

Sardinienregion

Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle

Etikett

Master resistivity curves for a two-, three-, and four-layer earth

"War against terrorism" is the new stage of the continuous war wich is waged with econimic, political and military means ..

A summary of the techniques of variable Mach number supersonic wind tunnel nozzle design

Two-dimensional wind tunnel wall interference

Fuori dal tunnel

None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

Two of a mind

A zed and two noughts : [original music from the film by Peter Greenaway]

Kommentare