Cryogenic wind tunnel research: a global perspectiveDRESS, D. A; KILGORE, R. A.Cryogenics (Guildford). 1988, Vol 28, Num 1, pp 10-21, issn 0011-2275Article

Code des singularités surfaciques pour calcul d'effets de parois et de supports de formes quelconques sur des maquettes en soufflerie = Vortex lattice code for computation of any wird tunnel and support effects on modelsVAUCHERET, X.La Recherche aérospatiale. 1991, Num 2, pp 39-51, issn 0034-1223, 13 p.Article

Détermination des pertubations des champs d'écoulements des souffleries supersoniques d'après les valeurs mesurées des coefficients aérodynamiquesEREMIN, V. V; LIPNITSKIJ, YU. M; FILIPPOV, S. E et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1988, Num 5, pp 183-185, issn 0568-5281Article

Two-dimensional wall adaption in the transonic windtunnel of the AIAROMBERG, H.-J.Experiments in fluids. 1990, Vol 9, Num 3, pp 177-180, issn 0723-4864, 4 p.Article

Die Messtechnik im Windkanal I der TU Dresden = The metrology in the wind-tunnel I of the Dresden University of TechnologySIEMENS, H.Wissenschaftliche Zeitschrift der Technischen Universität Dresden. 1989, Vol 38, Num 3, pp 85-88, issn 0043-6925, 4 p.Conference Paper

Exploratory flutter test in a cryogenic wind tunnelCOLE, S. R.Journal of aircraft. 1986, Vol 23, Num 12, pp 904-911, issn 0021-8669Article

Numerical simulation of the transonic DFLR-F5 wing experiment: Proceeding/International workshop «Numerical simulation of compressible viscous-Flow aerodynamics», Göttingen, September 30-October 2, 1987KORDULLA, W.Notes on numerical fluid mechanics. 1988, Vol 22, issn 0179-9614, 305 p.Conference Proceedings

Two-dimensional adaptive-wall tests in the NASA Ames two- by two-foot transonic wind tunnelSCHAIRER, E. T; LEE, G; MCDEVITT, T. K et al.Journal of aircraft. 1991, Vol 28, Num 11, pp 673-682, issn 0021-8669Article

Cryogenic transonic wind tunnels and the condensation of nitrogenWEGENER, P. P.Experiments in fluids. 1991, Vol 11, Num 5, pp 333-338, issn 0723-4864Article

Investigation of flow separation in a three-dimensional diffuser using a coupled Euler and boundary-layer methodSTOCK, H. W; LEICHER, S; SEIBERT, W et al.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1988, Vol 12, Num 5-6, pp 347-357, issn 0342-068XArticle

Disturbance of transonic wind tunnel flow by a slot in the tunnel wallRISTIC, S.Experiments in fluids. 1991, Vol 11, Num 6, pp 403-404, issn 0723-4864Article

Wind tunnel facility for operation at very low velocityLEITH, J. R; RAETHER, A. M; SMITH, D. K et al.Journal of physics. E. Scientific instruments. 1988, Vol 21, Num 5, pp 497-501, issn 0022-3735Article

Wave cancellation properties of a splitter-plate porous wall configurationELFSTROM, G. M; MEDVED, B; RAINBIRD, W. J et al.Journal of aircraft. 1989, Vol 26, Num 10, pp 920-924, issn 0021-8669, 5 p.Conference Paper

Acoustic levitation in a free-jet wind tunnelSEAVER, M; GALLOWAY, A; MANUCCIA, T. J et al.Review of scientific instruments. 1989, Vol 60, Num 11, pp 3452-3459, issn 0034-6748, 8 p.Article

Wind tunnel evaluation of an aircraft-borne sampling systemIRSHAD, Hammad; MCFARLAND, Andrew R; LANDIS, Matthew S et al.Aerosol science and technology. 2004, Vol 38, Num 4, pp 311-321, issn 0278-6826, 11 p.Article

New method for evaluating the hemispheric five-hole probesJUNNAI ZHAI; REBSTOCK, Ruediger; HUFNAGEL, Klaus et al.Journal of aircraft. 2006, Vol 43, Num 3, pp 855-858, issn 0021-8669, 4 p.Article

DARPA/AFRL/NASA Smart Wing second wind Tunnel test resultsSCHERER, L. B; MARTIN, C. A; WEST, M et al.SPIE proceedings series. 1999, pp 249-259, isbn 0-8194-3148-6Conference Paper

Strömungsakustische Modelluntosuchungen für einen Freistrahl-Windkanal = Aero-acoustic model-scale investigations on open-jet wind-tunnelsACKERMANN, V.Zeitschrift für Lärmbekämpfung. 1991, Vol 38, Num 1, pp 10-18, issn 0174-1098, 9 p.Article

Flow blockage in model testing in the perforated working section of a wind tunnel as M∞→1NEILAND, V. M; KHOZYAENKO, N. N.Fluid dynamics. 1991, Vol 26, Num 3, pp 443-448, issn 0015-4628Article

A non-integral, axial-force measuring elementRINGEL, M; LEVIN, D; SEGINER, A et al.Experiments in fluids. 1989, Vol 7, Num 1, pp 56-60, issn 0723-4864Article

Plannung eines Aero-Akustik-Windkanals = Planning of an aeroacoustic wind tunnel (SBI - prüfstands und industrie anlagen gesamtplannung)ATZ. Automobiltechnische Zeitschrift. 1996, pp 88-92, issn 0001-2785, 4 p., NSArticle

Overview of the DARPA/AFRL/NASA Smart Wing ProgramKUDVA, J. N; MARTIN, C. A; SCHERER, L. B et al.SPIE proceedings series. 1999, pp 230-236, isbn 0-8194-3148-6Conference Paper

Organisation de la maintenance préventive de la soufflerie climatique. Circuit thermique = Preventive maintenance of the climatic wind tunnel. Thermal circuitJARNAUD, D.1996, 56 p.Report

La soufflerie climatique Jules Verne. Notice sur les caractéristiques des écoulements obtenus dans les veines environnement et haute vitesse = The Jules Verne Climatic Wind Junnel. Data Sheet on the flow characteristics obtained in the environmental and high speed tunnelsDUFRESNE DE VIREL, M.1992, 20 p.Book

Aerodynamic data accuracy and quality: requirements and capabilities in wind tunnel testing: papers presented and discussions/Fluid dynamics Panel, symposium, Naples, ITA, 28 September-10 October 1987AGARD conference proceedings. 1988, Num 429, issn 0549-7191, 514 p.Conference Proceedings