Books on the topic 'Wind tunnel balance'

Britcher, Colin P. Application of magnetic suspension and balance systems to ultra-high Reynolds number facilities. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Britcher, Colin P. Applications of magnetic suspension technology to large scale facilities: Progress, problems and promises. [Washington, DC: National Aeronautics and Space Administration, 1997.

Johnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. Hampton, Va: Langley Research Center, 1989.

Johnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Johnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Johnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Johnson, William G. The 13-inch magnetic suspension and balance system wind tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Baljeu, J. F. Development of a multi-component internal strain-gauge balance for model tests in a cryogenic wind tunnel. Amsterdam: National Aerospace Laboratory, 1988.

Welsh, B. L. A dynamic balance for the measurement of time-dependent aerodynamic forces on wind-tunnel models. London: HMSO, 1990.

Huebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.

Hufnagel, Klaus. Wind Tunnel Balances. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97766-5.

Kniskern, Marc W. Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation. Raleigh, [N.C.]: North Carolina State University, Dept. of Mechanical and Aerospace Engineering, 1990.

Kniskern, Marc W. Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation. Raleigh, [N.C.]: North Carolina State University, Dept. of Mechanical and Aerospace Engineering, 1990.

Kniskern, Marc W. Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation. Raleigh, [N.C.]: North Carolina State University, Dept. of Mechanical and Aerospace Engineering, 1990.

Test of a trail [sic] cryogenic balance in the ONERA T2 wind tunnel. Washington, DC: National Aeronautics and Space Administration, 1987.

P, Boyden Richmond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Aerodynamic measurements and thermal tests of a strain-gage balance in a cryogenic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

W, Kniskern Marc, Monta William J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

W, Kniskern Marc, Monta William J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

National Aeronautics and Space Administration (NASA) Staff. Assessment of a Flow-Through Balance for Hypersonic Wind Tunnel Models with Scramjet Exhaust Flow Simulation. Independently Published, 2018.

Innovative Control Effectors (Configuration 101) Dynamic Wind Tunnel Test Report. Rotary Balance and Forced Oscillation Tests. Storming Media, 1998.

Techniques for extreme attitude suspension of a wind tunnel model in a magnetic suspension and balance system. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

Darmstadt, TU. Wind Tunnel Balances. Springer International Publishing AG, 2022.

S, Tripp John, Tcheng Ping, and Langley Research Center, eds. First International Symposium on Strain Gauge Balances. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Wayne, McKinney L., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Overview of the 1989 Wind Tunnel Calibration Workshop. Washington, DC: National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.

A, Kilgore Robert, Sych Karen L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Rotary balances: A selected, annotated bibliography. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Visual display and alarm system for wind tunnel static and dynamic loads. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

American Institute of Aeronautics and As. Recommended Practice: Calibration and Use of Internal Strain Gage Balances With Application to Wind Tunnel Testing (Aiaa Standards). AIAA (American Institute of Aeronautics & Ast, 2003.

American Institute of Aeronautics and As. Recommended Practice: Calibration and Use of Internal Strain-Gage Balances With Application to Wind Tunnel Testing (AIAA Standards). AIAA (American Institute of Aeronautics & Ast, 2004.

Cryogenic strain gage techniques used in force balance design for the National Transonic Facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Cryogenic strain gage techniques used in force balance design for the National Transonic Facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Center, Langley Research, ed. Cryogenic strain gage techniques used in force balance design for the National Transonic Facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

Center, Lewis Research, ed. Model engine performance measurement from force balance instrumentation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091A-2020). 12700 Sunrise Valley Drive, Suite 200, Reston, VA 20191: American Institute of Aeronautics and Astronautics, Inc., 2020. http://dx.doi.org/10.2514/4.106019.

Recommended Practice: Calibration and Use of Internal Strain-Gage Balances with Application to Wind Tunnel Testing (AIAA R-091-2003). Washington, DC: American Institute of Aeronautics and Astronautics, Inc., 2003. http://dx.doi.org/10.2514/4.476464.