Books on the topic 'Aerodynamic interference'

Baysal, Oktay. Supersonic aerodynamic interference effects of store separation. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1987.

West, Michael Gerard. Aerodynamic interference during air-to-air refuelling. Manchester: University ofManchester, 1993.

D. I. T. P. Llewelyn-Davies. The effect of pitch and yaw on the aerodynamic interference between two identical, unstaggered, axisymmetrical bodies whose centrelines are parallel and separated by 1.11 body diameters. Cranfield, Bedford, England: Cranfield Institute of Technology, College of Aeronautics, 1989.

Labrujere, Th E. Evaluation of measured-boundary-condition methods for 3D subsonic wall interference. Amsterdam: National Aerospace Laboratory, 1988.

Britcher, Colin P. Subsonic sting interference on the aerodynamic characteristics of a family of slanted-base ogive-cylinders. Hampton, Va: Langley Research Center, 1990.

Smith, J. 2D wall interference assessment using "Calspan Pipes". Amsterdam: National Aerospace Laboratory, 1985.

Labrujere, Th E. Correction for wall interference in a solid-wall wind tunnel using sparse measured boundary conditions. Amsterdam: National Aerospace Laboratory, 1989.

Smith, J. A transonic model representation for two-dimensional wall interference assessment. Amsterdam: National Aerospace Laboratory, 1986.

Pandey, Ajay K. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Goodyer, M. J. Derivation of jack movement influence coefficients as a basis for selecting wall contours giving reduced levels of interference in flexible walled test sections. Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, 1985.

Schairer, Edward T. A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Ulbrich, Norbert. Description of panel method code ANTARES. Moffett, Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2000.

Ulbrich, Norbert. Description of panel method code ANTARES. Moffett, Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2000.

Mineck, Raymond E. Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Mineck, Raymond E. Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques. Hampton, Va: Langley Research Center, 1992.

Mineck, Raymond E. Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section. Hampton, Va: Langley Research Center, 1987.

Mineck, Raymond E. Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Ulbrich, Norbert. The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Ulbrich, Norbert. The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Ulbrich, Norbert. The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Ulbrich, Norbert. The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Ulbrich, Norbert. The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

Center, Lewis Research, ed. A review of turbomachinery blade-row interaction research. Cleveland, Ohio: Lewis Research Center, National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

Ramesh, Pankajakshan, and United States. National Aeronautics and Space Administration., eds. Propulsion/airframe interference for ducted propfan engines with ground effect. [Washington, DC: National Aeronautics and Space Administration, 1994.

Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Computer simulation of a wind tunnel test section with discrete finite-length wall slots. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Center, Langley Research, ed. An experimental and analytical study of the aerodynamic interference effects between two Sears-Haack bodies at Mach 2.7. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

J, Verriere, Quemard G, and United States. National Aeronautics and Space Administration., eds. The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients. Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Final report, June 1991 - June 1994. Tullahoma, TN: Center for Space Transportation and Applied Research, 1994.

A wall interference assessment/correction system: Final report, June 1991 - June 1994. Tullahoma, TN: Center for Space Transportation and Applied Research, 1994.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #2, January - June 1992. Tullahoma, Tenn: University of Tennessee Space Institute, 1992.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #2, January - June 1992. Tullahoma, Tenn: University of Tennessee Space Institute, 1992.

A wall interference assessment/correction system: Semi-annual report #3, July - December 1992. Tullahoma, Tenn: University of Tennessee Space Institute, 1992.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #3, July - December 1992. Tullahoma, Tenn: University of Tennessee Space Institute, 1992.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #4, January-June 1993. Tullahoma, TN: CSTAR - Center for Space Transportation and Applied Research, 1993.

United States. National Aeronautics and Space Administration., ed. A wall interference assessment/correction system: Semi-annual report #4, January-June 1993. Tullahoma, TN: CSTAR - Center for Space Transportation and Applied Research, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987.

A wall interference assessment/correction system: Semi-annual report #1, covering the period June 1991 through December 1991. Tullahoma, Tenn: Center for Space Transportation and Applied Research, 1991.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Adaptive wall technology for minimization of wall interferences in transonic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Center, Langley Research, ed. Unsteady transonic flow calculations for wing-fuselage configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Pramote, Dechaumphai, Thornton Earl A. 1936-, and Langley Research Center, eds. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Pramote, Dechaumphai, Thornton Earl A. 1936-, and Langley Research Center, eds. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Pramote, Dechaumphai, Thornton Earl A. 1936-, and Langley Research Center, eds. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

A, Newman Perry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.