Books on the topic 'Static performance'

E, Reubush David, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Bangert, Linda S. Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

L, Mason Mary, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Static performance of an axisymmetric nozzle with post-exit vanes for multiaxis thrust vectoring. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

W, Schirmer Alberto, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

C, Pendergraft Odis, and Langley Research Center, eds. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

C, Pendergraft Odis, and Langley Research Center, eds. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Foley, Robert J. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes. Langley Research Center, 1991.

C, Asbury Scott, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

D, Leavitt Laurence, та United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ред. Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60ʻ́. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Dubé, Jean-Pierre. Improving the numerical performance of blp static and dynamic discrete choice random coefficients demand estimation. National Bureau of Economic Research, 2009.

C, Hendricks Robert, Yoder Dennis A, and United States. National Aeronautics and Space Administration., eds. Brush seal leakage performance with gaseous working fluids at static and low rotor speed condtitions. National Aeronautics and Space Administration, 1992.

H, Klyde David, and Langley Research Center, eds. Tailless aircraft performance improvements. National Aeronautics and Space Administration, Langley Research Center, 1989.

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. Space shuttle production verification motor-1 (PV-1) static fire.: Final test report. Thiokol Corp., Space Operations, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Bare, E. Ann. Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters. Langley Research Center, 1989.

J, McDonald Timothy, and NASA Glenn Research Center, eds. Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations. National Aeronautics and Space Administration, Glenn Research Center, 2001.

Leavitt, Laurence D. Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities. NASA, 1985.

A, Hunter Craig, and Langley Research Center, eds. Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control. National Aeronautics and Space Administration, Langley Research Center, 1999.

Asbury, Scott C. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. Langley Research Center, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

D, Leavitt Laurence, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Center, Langley Research, ed. An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles. National Aeronautics and Space Administration, Langley Research Center, 1995.

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Hendricks, Robert C. Three-step labyrinth seal for high-performance turbomachines. Lewis Research Center, 1987.

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. QM-8 final performance evaluation report. Thiokol Corp., Space Operations, 1989.

Operations, Thiokol Corporation Space, and George C. Marshall Space Flight Center., eds. QM-8 final performance evaluation report. Thiokol Corp., Space Operations, 1989.

United States. National Aeronautics and Space Administration., ed. SUBSONIC MANEUVERING EFFECTIVENESS OF HIGH PERFORMANCE AIRCRAFT WHICH EMPLOY QUASI-STATIC SHAPE CHANGE... NASA/TM-1998-207570... MAY 5, 1998. s.n., 1999.

A, Yetter Jeffrey, and Langley Research Center, eds. Static performance of six innovative thrust reverser concepts for subsonic transport applications: Summary of the NASA Langley Innovative Thrust Reverser Test Program. National Aeronautics and Space Administration, Langley Research Center, 2000.

N, Berger Allen, and World Bank, eds. Corporate governance and bank performance: A joint analysis of the static, selection, and dynamic effects of domestic, foreign, and state ownership. World Bank, 2005.

Wilkinson, John P. Space shuttle production verification motor 1 (PV-1) field joint protection system.: Final report. Thiokol Corp., Space Operations, 1990.

Italy) Corpo in performance tra stati di alterazione di coscienza e processo creativo (Conference) (2019 Bologna. Il corpo in performance: Tra stati di alterazione di coscienza e processo creativo. Mimesis, 2020.

Heckman, James J. The performance of performance standards. National Bureau of Economic Research, 2002.

Stone, Sara Jane. Command performance. Harlequin, 2013.

Gerald, Miller, Hildreth W. Bartley 1949-, and Rabin Jack 1945-, eds. Performance-based budgeting. Westview Press, 2001.

United States. General Accounting Office. Accounting and Financial Management Division, ed. IRS performance measures. The Office, 1992.

Blunt, Janet H. Computerized performance testing as a surrogate job performance measure. Air Force Human Resources Laboratory, Air Force Systems Command, 1989.

Division, United States General Accounting Office Accounting and Financial Management. IRS performance measures. The Office, 1992.

1929-, Steinberg Marvin B., American Bar Association, and National Conference of State Trial Judges (U.S.). Committee on Evaluation of Judicial Performance., eds. Judicial performance evaluation handbook. The Association, 1996.

1929-, Steinberg Marvin B., and National Conference of State Trial Judges (U.S.). Committee on Evaluation of Judicial Performance., eds. Judicial performance evaluation handbook. The Association, 1996.

Hauser, W. Kurt. Taxation and economic performance. Hoover Institution on War, Revolution, and Peace, Stanford University, 1996.

Void, Joyce D. Aircraft performance: Flying training. Dept. of the Air Force, Headquarters US Air Force, 1990.