Seguici su

Cerca

Torna Indietro

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

Schurmeier, H. M.

Informazioni

Lo trovi in

Categoria

Testo

Natura

Monografia

Titolo

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

Nomi

[Autore] Schurmeier, H. M.
AGARD

Descrizione

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

Descrizione Fisica

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

Data

1959

Luogo di pubblicazione

Paris

Paese

FRANCIA

Lingua

INGLESE

Fonte

Biblioteche SBN Sardegna

ID

IT\ICCU\RMS\1096810

Link Risorse

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

Tag

Immagini

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

Autore : Mooney, Harold Morton

Anno : 1956

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

Anno : 2001

Risultati 2 di 83799

Visualizza Tutti

Testi

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

Autore : Kenney, J. T.

Anno : 1954

Two-dimensional wind tunnel wall interference

Autore : Mokry, M.

Anno : 1983

Risultati 2 di 2187115

Visualizza Tutti

Video

Fuori dal tunnel

Anno : 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)

Anno : 1990

Risultati 2 di 70636

Visualizza Tutti

Audio

Two of a mind

Autore : Desmond, Paul

Anno : 2010

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

Autore : Nyman, Michael

Anno : 2004

Risultati 2 di 25642

Visualizza Tutti

Commenti

Carica altri

Scrivi un commento

Invia

Regione Sardegna

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

Tag

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]

Commenti