The Locator -- [(subject = "Angle of attack")]

The Locator -- [(subject = "Angle of attack")]

110 records matched your query

Record 1: Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds Format: [microform] / Author: Kim, Hyun D. Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Date: [2001] This title can be found in 1 Iowa libraries.
Record 2: Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees Format: [microform] / Author: Prabhu, Ramadas K. Publisher: Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Date: [2001] This title can be found in 1 Iowa libraries.
Record 3: Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates Format: [microform] / Author: Lliff, Kenneth W. Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Date: [1999] This title can be found in 2 Iowa libraries.
Record 4: Flight test of an adaptive configuration optimization system for transport aircraft Format: [microform] / Author: Gilyard, Glenn B. Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Date: 1999] This title can be found in 1 Iowa libraries.
Record 5: Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft Format: [microform] / Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Date: [1999] This title can be found in 1 Iowa libraries.
Record 6: Navier-Stokes simulation of several high-lift reference H configurations Format: [microform] / Author: Lessard, Wendy B. Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: 1999] This title can be found in 2 Iowa libraries.
Record 7: Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Format: [microform] : Author: Moses, Robert W. Publisher: Reston, Va. : American Institute of Aeronautics and Astronautics ; Date: 1998] This title can be found in 2 Iowa libraries.
Record 8: Design and performance calculations of a propeller for very high altitude flight Format: [microform] / Author: Koch, L. Danielle. Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Date: 1998] This title can be found in 2 Iowa libraries.
Record 9: Two-dimensional high-lift aerodynamic optimization using neural networks Format: [microform] / Author: Greenman, Roxana M. Publisher: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 10: Experimental and theoretical study of flow fields around ducted-nacelle models Format: [microform] / Author: Mack, Robert J. Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: 1998] This title can be found in 1 Iowa libraries.
Record 11: Global artificial boundary conditions for computation of external flow problems with propulsive jets Format: [microform] / Publisher: Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 12: Reynolds number effects at high angles of attack Format: [microform] / Publisher: Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 13: A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane Format: [microform] / Author: Lallman, Frederick J. Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 14: Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models Format: [microform] / Author: Charlton, Eric F. Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 15: High-alpha research vehicle lateral-directional control law description, analyses, and simulation results Format: [microform] / Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 16: Mechanical design of high lift systems for high aspect ratio swept wings Format: [microform] / Author: Rudolph, Peter K. C. Publisher: Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Date: 1998] This title can be found in 2 Iowa libraries.
Record 17: Computational/experimental aeroheating predictions for X-33 phase II vehicle Format: [microform] / Publisher: Reston, VA : American Institute of Aeronautics and Astronautics ; Date: 1998] This title can be found in 2 Iowa libraries.
Record 18: Euler technology assessment SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts / Format: [microform] : Author: Jordan, Keith J. Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 19: Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18 Format: [microform] / Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1998] This title can be found in 2 Iowa libraries.
Record 20: Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel Format: [microform] / Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Date: [1997] This title can be found in 1 Iowa libraries.

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