Active filters
Displaying 21 of 21 results
Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle [microform] / William Herkes.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 2000-
2000
0 resources
Noise measurements from an ejector suppressor nozzle in the NASA Lewis 9- by 15-foot low speed wind tunnel [microform] / Eugene A. Krejsa ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
A control-volume method for analysis of unsteady thrust augmenting ejector flows [microform] / Colin K. Drummond.
Text
Cleveland, Ohio : Lewis Research Center, National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]
1988
0 resources
Experiments on high speed ejectors [microform] / J.J. Wu.
Text
[Moffett Field, Calif.] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft [microform] / David J. Anderson, Heather H. Lambert, and Masashi Mizukami.
Text
[Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
1992
0 resources
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight [microform] / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Lobed mixer optimization for advanced ejector geometries [microform] : annual report and proposal for continuation of NASA contract NCC3-414 / principal investigator: Ian A. Waitz.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows [microform] : prepared under grant NGT-51244 / Lawrence Justin De Chant.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Analysis of a rocket based combined cycle engine during rocket only operation [microform] / T.D. Smith ... [et al.].
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system [microform] / Nicholas J. Georgiadis, James F. Walker, and Charles J. Trefny.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Effect of delta tabs on free jets from complex nozzles [microform] / K.B.M.Q Zaman.
Text
[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 requiredUnsteady ejector performance [microform] : an experimental investigation using a pulsejet driver / Daniel E. Paxson, Jack Wilson and Kevin T. Dougherty.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
2002
1 resource
Available online
Adobe Acrobat Reader requiredThrust augmentation measurements using a pulse detonation engine ejector [microform] / Robert J. Santoro and Sibtosh Pal.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
2003
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS55218Supersonic STOVL aircraft from a propulsion point of view [microform] / R. Luidens, ... [et al.].
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS99449Experimental investigation of an ejector-powered free-jet facility [microform] / Mary Jo Long.
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1992]
1992
0 resources
Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1997.
1997-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo72111Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
2002-10
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS53266Effect of delta tabs on free jets from complex nozzles / K.B.M.Q. Zaman.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2001.
2001-3
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS26802A multidisciplinary approach to mixer-ejector analysis and design / Eric S. Hendricks and Jonathan A. Seidel.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo33020No results found from Digital Research Books Beta
Digital books for research from multiple sources worldwide - all free to read, download, and keep. No library card required.
Explore Digital Research Books Beta