Книги з теми "Yawing moment"

Cobleigh, Brent R. Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.

Messina, Michael D. Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

A, Croom Mark, and Dryden Flight Research Facility, eds. Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.

A, Croom Mark, and Dryden Flight Research Facility, eds. Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.

A, Croom Mark, and Dryden Flight Research Facility, eds. Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 2001.

United States. National Aeronautics and Space Administration., ed. Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail. [Washington, DC: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail. [Washington, DC: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. Sailplane glide performance and control using fixed and articulating winglets: A thesis. [Washington, DC: National Aeronautics and Space Administration, 1995.

Center, Ames Research, ed. Numerical analysis of tangential slot blowing on a generic chined forebody. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

J, O'Rourke Matthew, and Langley Research Center, eds. Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

H, Starnes James, United States. National Aeronautics and Space Administration., and AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (1998 Long Beach, Calif.), eds. Effect of curvature on the impact damage characteritiscs and residual strength of composite plates: Presented at 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : Long Beach, California, April 20-23, 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

Hugh L. Dryden Flight Research Center., ed. High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.

High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.

Hugh L. Dryden Flight Research Center., ed. High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1994.

G, Murri Daniel, Lanser Wendy R, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

G, Murri Daniel, Lanser Wendy R, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

N, Pedreiro, Joint Institute for Aeronautics and Acoustics., and United States. National Aeronautics and Space Administration., eds. Roll-yaw control at high angle of attack by forebody tangential blowing. [Stanford, Calif.?]: Joint Institute for Aeronautics and Acoustics, 1995.

United States. National Aeronautics and Space Administration., ed. Computational analysis of forebody tangential slot blowing on the high alpha research vehicle. San Jose, CA: MCAT Institute, 1995.

United States. National Aeronautics and Space Administration., ed. Computational analysis of forebody tangential slot blowing on the high alpha research vehicle. San Jose, CA: MCAT Institute, 1994.