Książki na temat „Stability of Ankle”

Jorden, Frank L. Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane. Langley Research Center, 1992.

E, Hahne David, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Wind-tunnel static and free-flight investigation of high-angle-of-attack stability and control characteristics of a model of the EA-6B airplane. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

E, Hahne David, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Wind-tunnel static and free-flight investigation of high-angle-of-attack stability and control characteristics of a model of the EA-6B airplane. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1996.

Ndaona, Chokani, and Langley Research Center, eds. Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel. National Aeronautics and Space Administration, Langley Research Center, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, 1996.

Charles, Wang Kon-Sheng, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Brandon, Jay M. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. Langley Research Center, 1986.

Center, Langley Research, ed. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Center, Langley Research, ed. Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1997.

United States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.

United States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.

United States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. American Institute of Aeronautics and Astronautics, 1995.

E, Hahne David, Cockrell Charles E, and United States. National Aeronautics and Space Administration., eds. Low-speed wind tunnel tests of two waverider configuration models. American Institute of Aeronautics and Astronautics, 1995.

Eli, Reshotko, American Institute of Aeronautics and Astronautics., and Lewis Research Center, eds. Physical mechanisms of glaze ice scallop formations on swept wings. National Aeronautics and Space Administration, Lewis Research Center, 1998.

George C. Marshall Space Flight Center., ed. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

Charles, Wang Kon-Sheng, and Hugh L. Dryden Flight Research Center., eds. 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. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

P, Gilbert William, Anglin Ernie L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Charles, Wang Kon-Sheng, and Hugh L. Dryden Flight Research Center., eds. 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. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Charles, Wang Kon-Sheng, and Hugh L. Dryden Flight Research Center., eds. 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. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. National Aeronautics and Space Administration, Langley Research Center, 1997.

Hahne, David E. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept. National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept. National Aeronautics and Space Administration, Langley Research Center, 1997.

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

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models. National Aeronautics and Space Administration, Langley Research Center, 1998.

Iliff, Kenneth W. 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 derivatives. National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

M, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.

M, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.

M, Moul Thomas, and United States. National Aeronautics and Space Administration., eds. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊. National Aeronautics and Space Administration, 1995.

Fears, Scott P. Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50. Langley Research Center, 1995.