|
|
 |
 |
|
|
|
Selected Navigations:
Author >
[x]
|
Sort results by:
|
|
|
There are a total of 9 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
|
Comparisons of theoretical and experimental pressure distributions on an arrow-wing configuration at transonic speed
Author(s): Manro, M. E.; Tinoco, E. N.; Bobbitt, P. J.; Rogers, J. T.
Abstract: A wind-tunnel test of an arrow-wing-body configuration employing both a twisted and a flat wing, as well as a variety of leading- and trailing-edge flap deflections, was conducted to provide an experimental data base for ...
NASA Center: Langley Research Center
Publication Year: 1975
Added to NTRS: 2008-11-10
Accession Number: 76N10049; Document ID: 19760002961
Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane
Author(s): Kuhl, A. E.; Little, M. V.; Rogers, J. T.
Abstract: Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplane
NASA Center: Dryden Flight Research Center
Publication Year: 1958
Added to NTRS: 2006-11-06
Accession Number: 66N39617; Document ID: 19660030327; Report Number: NACA-RM-H57C25
Comparisons of theoretical and experimental pressure distributions on an arrow-wing configuration at subsonic, transonic, and supersonic speeds
Author(s): Manro, M. E.; Bobbitt, P. J.; Rogers, J. T.
Abstract: A wind tunnel test of an arrow wing body configuration consisting of flat and twisted wings, as well as a variety of leading- and trailing-edge control surface deflection, has been conducted at Mach numbers from 0.40 to 2.50 ...
NASA Center: Langley Research Center
Publication Year: 1977
Added to NTRS: 2006-08-02
Accession Number: 77N20000; Document ID: 19770013056
Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration
Author(s): Manro, M. E.; Manning, K. J. R.; Hallstaff, T. H.; Rogers, J. T.
Abstract: A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to ...
NASA Center: NASA (non Center Specific)
Publication Year: 1976
Added to NTRS: 2005-10-13
Accession Number: 76N32132; Document ID: 19760025044; Report Number: D6-42670-1, FAA-RD-76-72, NASA-CR-2610
Summary report of the Aircraft Design Committee
Author(s): Rogers, J. T.
Abstract: Aircraft models were designed to solve aircraft lightning, severe storms, turbulence, icing, and visibility problems. Analytical modeling, wind tunnel simulation tests, ground tests, and in-flight tests were conducted.
NASA Center: NASA (non Center Specific)
Publication Year: 1978
Added to NTRS: 2005-08-25
Accession Number: 79N17430; Document ID: 19790009259
Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration. Volume 2: Experimental data report, effects of control surface deflection
Author(s): Manro, M. E.; Manning, K. J. R.; Hallstaff, T. H.; Rogers, J. T.
Abstract: For abstract, see N76-11034.
NASA Center: NASA (non Center Specific)
Publication Year: 1975
Added to NTRS: 2004-11-03
Accession Number: 76N11035; Document ID: 19760003947; Report Number: D6-42670-3-VOL-2, NASA-CR-132728
Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration. Volume 3: Data report, comparison of attached flow theories to experiment
Author(s): Manro, M. E.; Manning, K. J. R.; Hallstaff, T. H.; Rogers, J. T.
Abstract: For abstract, see N76-11034.
NASA Center: NASA (non Center Specific)
Publication Year: 1975
Added to NTRS: 2004-11-03
Accession Number: 76N11036; Document ID: 19760003948; Report Number: D6-42670-4-VOL-3, NASA-CR-132729
Requirements for implementation of Kuessner and Wagner indicial lift growth functions into the FLEXSTAB computer program system for use in dynamic loads analyses
Author(s): Miller, R. D.; Rogers, J. T.
Abstract: General requirements for dynamic loads analyses are described. The indicial lift growth function unsteady subsonic aerodynamic representation is reviewed, and the FLEXSTAB CPS is evaluated with respect to these general ...
NASA Center: NASA (non Center Specific)
Publication Year: 1975
Added to NTRS: 2004-11-03
Accession Number: 76N14047; Document ID: 19760006959; Report Number: NASA-CR-137718
Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration. Volume 1: Experimental data report, base configuration and effects of wing twist and leading-edge configuration
Author(s): Manro, M. E.; Manning, K. J. R.; Hallstaff, T. H.; Rogers, J. T.
Abstract: A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings, as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to ...
NASA Center: NASA (non Center Specific)
Publication Year: 1975
Added to NTRS: 2004-11-03
Accession Number: 76N11034; Document ID: 19760003946; Report Number: D6-42670-2-VOL-1, NASA-CR-132727
|
|
|
|
|
