The Online Books Page

Online Books by

Howard W. Stone

Books from the extended shelves:

• Stone, Howard W.: Analysis of the space shuttle orbiter entry dynamics from Mach 10 to Mach 2.5 with the November 1976 flight control system / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1980), also by Richard W. Powell and Langley Research Center (page images at HathiTrust)
• Stone, Howard W.: Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), also by Lawrence F. Rowell, Richard W. Powell, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stone, Howard W.: Effect of aerodynamic and angle-of-attack uncertainties on the blended entry flight control system of the space shuttle from Mach 10 to 2.5 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), also by Richard W. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Stone, Howard W.: Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the space shuttle from Mach 8 to 1.5 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985), also by Richard W. Powell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Stone, Howard W.: Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967), also by James C. Dunavant, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Stone, Howard W.: Effects of modifications to the space shuttle entry guidance and control systems / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), also by Richard W. Powell, Lawrence F. Rowell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Stone, Howard W.: Entry dynamics of space shuttle orbiter with lateral-directional stability and control uncertainties at supersonic and hypersonic speeds / ([Washington] : National Aeronoautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by Richard W. Powell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Stone, Howard W.: Entry dynamics of space shuttle orbiter with longitudinal stability and control uncertainties at supersonic and hypersonic speeds / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), also by Richard W. Powell, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Stone, Howard W.: The leading-edge effects on the laminar flat-plate boundary layer and the aerodynamic heating at Mach 10.4 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)

See also what's at your library, or elsewhere.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.