出版: | [Washington : For sale by the Supt. of Docs., U.S. Govt. Print. Off. |
出版: | Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Chiefly statistical tables. Prepared at Langley Research Center. "September 1969." Cover title. Includes bibliographical references (p. 3). Airplane response to ground roughness from three-track runway and taxiway profiles by elevation angle measurements. |
出版: | Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230] : National Aeronautics and Space Administration |
附註: | Includes bibliographical references (p. 13). |
出版: | Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Prepared at Goddard Space Flight Center. "August 1969"--Cover. Includes bibliographical references (p. 8). |
出版: | Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] : National Aeronautics and Space Administration |
附註: | Includes bibliographical references (p. 16-17). Pressure and heat transfer on swept delta wing with trailing-edge flap. |
出版: | Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Prepared at Lewis Research Center. "September 1969"--Cover. Includes bibliographical references (p. 23). |
出版: | Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151] |
附註: | Includes bibliographical references (p. 15). Incompressible approximation solution of additive drag coefficient and mass flow ratio for inlets with right circular cones. |
出版: | Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Prepared at Lewis Research Center. "August 1969"--Cover. Includes bibliographical references (p. 87). |
出版: | Upton, N.Y. : Brookhaven National Laboratory |
附註: | "October 1969." Includes bibliographical references (p. 37-39).31 |
出版: | Fort Collins, Colo. : Rocky Mountain Forest and Range Experiment Station, Forest Service, U.S. Dept. of Agriculture |
附註: | Caption title. |
出版: | Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230] : National Aeronautics and Space Administration |
附註: | Includes bibliographical references (p. 9-10). Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees. |
出版: | Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Prepared at Langley Research Center. "December 1969." Cover title. Includes bibliographical references (p. 12). Heat transfer measurements at Mach 10 on total angle cone downstream of air and helium transpiration cooling region. Also issued online. |
出版: | Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] |
附註: | Includes bibliographical references (p. 39). Injection of attached inviscid jet at oblique angle to moving stream. |
出版: | Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151] : National Aeronautics and Space Administration |
附註: | Includes bibliographical references (p. 70). Analytical solution for inviscid separated jet injection at oblique angle into moving stream. |
出版: | Washington, D.C. : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] : National Aeronautics and Space Administration |
附註: | Includes bibliographical references (p. 14). Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies. |
出版: | Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] |
附註: | Includes bibliographical references (p. 8). Aerodynamic characteristics of large-angle cones in supersonic lifting capabilities. |
出版: | Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151] |
附註: | Includes bibliographical references (p. 24). Numerical analysis of laminar and turbulent mixing region for two dimensional jet injected at angle to moving stream. |
出版: | Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information |
附註: | Prepared at Ames Research Center. "November 1969." Cover title. Includes bibliographical references (p. 6-7). Heat-transfer rates were measured on large-angle conical bodies with large half-angles between 50 degrees and 90 degrees, at angles of attack from 0 degrees. The results at 0 degree angle of attack were predicted with Lees' similarity theory, using calculated flow properties at the boundary-layer edge. The calculated flow properties were obtained from Newtonian theory for the 50 degree cone and from a one- or two-strip solution using the method of integral relations for other cones. At 0 degree angle of attack, an increase in cone angle resulted in a decrease in the heating rate over much of the body. However, high heating rates occurred at the shoulder of the both the half-angle = 80 degree and half-angle =90 degree shapes because of local pressure gradients. On the windward side of the cones, the heating rate increased with angle of attack. |