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Entwicklung von Plasmabrennern für Luftbetrieb zum Einsatz in Raumfahrt-Versuchsanlagen. Von R. Gebel. Mit 117 Abb.
Book/Text
(München, Zentralstelle f. Luftfahrtdokumentation u. -information) 1969.
1969
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberJSG 81-1 | Item locationOffsite |
The Peenemünde wind tunnels : a memoir / Peter P. Wegener.
Book/Text
New Haven : Yale University Press, c1996.
1996
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberJSE 96-1275 | Item locationOffsite |
High-speed wind tunnel testing [by] Alan Pope [and] Kennith L. Goin.
Book/Text
New York, Wiley [1965]
1965
1 item
| Format | Call number | Item location |
|---|---|---|
| FormatBook/Text | Call numberVDY (Pope, A. High speed wind tunnel testing) | Item locationOffsite |
Engine component instrumentation development facility at NASA Lewis Research Center [microform] / Robert J. Bruckner, Alvin E. Buggele, and Jan Lepicovsky.
Microform
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] / Stephen W.D. Wolf.
Microform
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1992]
1992
0 resources
Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel [microform] / E. Allen Arrington and Mark T. Pickett.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel [microform] / Ronald H. Soeder.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
1992
0 resources
Results of a FRSI material test under Space Shuttle ascent conditions in the Ames Research Center SX7 foot supersonic wind tunnel [microform] / by P.L. Lemoine, J.G.R. Collette.
Microform
Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual [microform] / Ronald H. Soeder.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
CNSFV code development, virtual zone Navier-Stokes computations of oscillating control surfaces and computational support of the laminar flow supersonic wind tunnel [microform] / Goetz H. Knopfler.
Microform
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Method of characteristics design of a supersonic wind tunnel nozzle with square cross-section [microform] : status report for NASA Langley grant NAG-1-113, supplement 3 / principal investigator: Steven P. Schneider.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] / Stephen W.D. Wolf.
Microform
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1992]
1993
0 resources
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] / Dr. Stephen D. Wolf.
Microform
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration : National Technical Information Service, distributor, 1991]
1991
0 resources
Improved pressure measurement system for calibration of the NASA LeRC 10x10 supersonic wind tunnel [microform] / Philip Z. Blumenthal andStephen M. Helland.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
NASA Lewis wind tunnel model systems criteria [microform] / Ronald H. Soeder and Henry C. Haller.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A supersonic tunnel for laser and flow-seeding techniques [microform] / Robert J. Bruckner and Jan Lepicovsky.
Microform
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Review of aeronautical wind tunnel facilities [microform] / Committee on Assessment of National Aeronautical Wind Tunnel Facilities, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.
Microform
Washington, D.C. : National Academy Press ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
1988
0 resources
Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel [microform] / Mark A. Motter.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers [microform] / George L. Stefko and Robert J. Jeracki.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
1985
0 resources
Improved speed control system for an 87,000 hp wind tunnel drive [microform] / Edward A. Becks, Timothy J. Bencic, Philip Z. Blumenthal.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic laminar flow control research [microform] : semi-annual report #2, July 1994 - December 1994 / C.F. Lo, principal investigator.
Microform
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research [microform] : final report / Steven P. Schneider.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Supersonic laminar flow control research [microform] : semiannual report #2 / Dr. C.F. Lo, principal investigator.
Microform
Moffett Field, Calif. : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Computational support of the lamimar [i.e. laminar] supersonic wind tunnel, CNSFV code development, Maglev, and grid generation [microform] / Goetz H. Klopfer.
Microform
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic quiet-tunnel development for laminar-turbulent transition research [microform] : final report for NASA Langley grant NAG-1-1607 / Steven P. Schneider.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.
Microform
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Design and testing of an oblique all-wing supersonic transport [microform] / Christopher A. Lee.
Microform
San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
User manual for NASA Lewis 10- by 10-foot supersonic wind tunnel [microform] / Ronald H. Soeder.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Supersonic laminar flow control research [microform] : semiannual report #4, July 1995-December 1995 / C.F. Lo, principal investigator.
Microform
Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Instantaneous flow measurements in a supersonic wind tunnel using spectrally resolved Rayleigh scattering [microform] / Richard G. Seasholtz, Alvin E. Buggele, and Mark F. Reeder.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10̊ cone at Mach 1.6 [microform] / Stephen W.D. Wolf, James A. Laub.
Microform
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
An experimental device for generating high frequency perturbations in supersonic wind tunnels [microform] / Kevin J. Melcher and Mounir B. Ibrahim.
Microform
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Low speed calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1995 test) [microform] : under contract NAS3-27186 / E. Allen Arrington and Jose C. Gonsalez.
Microform
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Baseline calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1991 and 1992 tests) [microform] / E. Allen Arrington, Mark T. Pickett and Ronald H. Soeder.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, [1998]
1998
0 resources
Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel [microform] / E. Allen Arrington, Jose C. Gonsalez, and Edward A. Becks.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Subsonic flow quality surveys of the NASA Lewis Research Center 10- by 10-foot supersonic wind tunnel [microform] / E. Allen Arrington and Jose C. Gonsalez.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
1998
0 resources
Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test) [microform] / E. Allen Arrington.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
1998
0 resources
Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21) [microform] / A.M. Springer.
Microform
[Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
1998
0 resources
NASA Glenn 1-by 1-foot supersonic wind tunnel user manual [microform] / Kirk D. Seablom ... [et al.].
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Pressure probe designs for dynamic pressure measurements in a supersonic flow field [microform] / A. Robert Porro.
Microform
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
2001
1 resource
Available online
Adobe Acrobat Reader requiredResults of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C) [microform] / J. Marroquin.
Microform
Houston, Tex. : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.
1985
0 resources
Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data [microform] / D.R. Reddy and T.J. Benson and L.J. Weir ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Society of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 1990.
Microform
[Washington, D.C.] : NASA ; Springfield, Va. : For sale by the National Technical Information Service, [1990]
1990
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS69416Current wind tunnel capability and planned improvements at Lewis Research Center [microform] / David N. Bowditch.
Microform
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
1986
0 resources
Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface [microform] / V.P. Maksimov and A.A. Maslov.
Microform
Washington, D.C. : National Aeronautics and Space Administration, [1983]
1983
0 resources
Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) / E. Allen Arrington.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2011
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo27462Analysis of buzz in a supersonic inlet / Rodrick V. Chima.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo30597Wind tunnel testing of a one-dimensional laser beam scanning and laser sheet approach to shock sensing / Roger Tokars ... [and others].
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo32157Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / Randy Thomas and Thomas J. Stueber.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
2013-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo49566Investigation of materials for boundary layer control in a supersonic wind tunnel / Alexander C. Braafladt, John M. Lucero and Stefanie M. Hirt.
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2013.
2013-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo50546Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / Raymond Castner [and three others].
Web Resource
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
2013-7
1 resource
Available online
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