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Computational methods for HSCT-inlet controls/CFD interdisciplinary research [microform] / Gary L. Cole ... [et al.].
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions [microform] / Kamlesh Kapoor, Bernard H. Anderson.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application [microform] / Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
On supersonic-inlet boundary-layer bleed flow [microform] / Gary J. Harloff and Gregory E. Smith.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Computation of multi-dimensional viscous supersonic jet flow [microform] / Y.N. Kim, R.C. Buggeln, and H. McDonald ; prepared for Lewis Research Center under contract NAS3-22759.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
1986
0 resources
Large perturbation flow field analysis and simulation for supersonic inlets [microform] : final report / by M.O. Varner ... [et al.].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
1984
0 resources
Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet [microform] / M. Mizukami and J.D. Saunders.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.
Text
[Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Numerical simulation of supersonic and hypersonic inlet flow fields [microform] : final report / D. Scott McRae.
Text
Raleigh, N.C. : Mars Mission Research Center, North Carolina State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Axisymmetric inlet minimum weight design method [microform] / Shari-Beth Nadell.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Minimum weight design of a generic axisymmetric inlet [microform] / Shari-Beth Nadell.
Text
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct [microform] / Milo D. Dahl.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Joint US/Russia TU-144 engine ground tests [microform] / Waldo A. Acostia ... [et al.].
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Comparison of the aeroacoustics of two small-scale supersonic inlets [microform] : final technical report, NASA contract #--NAG 3-1539 / principal investigator, Wing Ng.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
A method for generating reduced order linear models of supersonic inlets [microform] : under grant NAG3-1450 / Amy Chicatelli and Tom T. Hartley.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
A method for generating reduced-order linear models of multidimensional supersonic inlets [microform] / Amy Chicatelli and Tom T. Hartley.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations [microform] : final technical report / Miklos Sajben, Donald D. Freund.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
Analysis of inlet-compressor acoustic interactions using coupled CFD codes [microform] / A. Suresh ... [et al.].
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
1998
0 resources
The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport [microform] / David Soreide, Rodney K. Bogue, Jonathan Seidel.
Text
[Edwards, Calif.] : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
1999
0 resources
Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows [microform] / John W. Slater.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2002]
2002
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS55081Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets [microform] / Charles J. Trefny and Joseph W. Wasserbauer.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
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.
Text
[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/LPS69416Three-dimensional viscous design methedology for advanced technology aircraft supersonic inlet systems [microform] / Bernhard H. Anderson.
Text
[Washington, D.C. : National Aeronautics and Space Administration, 1984]
1984
0 resources
Air intakes for a probative missile of rocket ramjet [microform] / G. Laruelle.
Text
Washington, D.C. : National Aeronautics and Space Administration, [1984]
1984
0 resources
Research on supersonic inlet bleed / David O. David, Manan A. Vyas, and John W. Slater.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo32068Design and analysis tool for external-compression supersonic inlets / John W. Slater.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo32321Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / Bobby W. Sanders.
Text
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
1980-1
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo52217Minimum weight design of a generic axisymmetric inlet / Shari-Beth Nadell.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
1996-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo67123The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / Milo D. Dahl.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
1996-11
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo70672Joint US / Russia TU-144 engine ground tests / Waldo A. Acosta [and four others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, June 1997.
1997-6
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo73193Shock generation and control using DBD plasma actuators : SBIR phase I final report / by Mehul P. Patel [and four others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo32876Investigation of two bifurcated-duct inlet systems from Mach 0 to 2.0 over a wide range of angles of attack / Eldon A. Latham.
Text
Moffett Field, California : Ames Research Center, May 1976.
1976-5
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo171204No results found from Digital Research Books Beta
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