LEADER 01833nam  22004337a 4500001    ocm41603953
003    OCoLC
005    20160802103042.0
008    990624s1999    ohu     b    f000 0 eng d
035    (Sirsi) o41603953
035    (OCoLC)41603953
040    GPO |cGPO |dDLC |dMvI |dUtOrBLW
049    ERE$
074    0830-D (MF)
086 0  NAS 1.15:208896
245 03 An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft / |cA. Reehorst [and others].
260    [Cleveland, Ohio] : |bNational Aeronautics and Space Administration, Lewis Research Center ;[Springfield, Va.] : |b[National Technical Information Service, distributor], |c[1999]
300    1 volume.
336    text |2rdacontent
337    microform |2rdamedia
338    microfiche |2rdacarrier
490 1  NASA TM- ; |v1999-208896
500    Shipping list no.: 99-0559-M.
533     |3Joyner-Microfiche. |b[Washington, D.C. : |cNational Aeronautics and Space Administration, |d1999] |e1 microfiche.
650  7 Aircraft icing. |2nasat
650  7 Aircraft control. |2nasat
650  7 Wind tunnel tests. |2nasat
650  7 Computational fluid dynamics. |2nasat
650  7 Navier-Stokes equation. |2nasat
650  7 Aircraft performance. |2nasat
650  7 Aerodynamic characteristics. |2nasat
700 1  Reehorst, A. |?UNAUTHORIZED
710 2  Lewis Research Center. |=^A367825
710 1  United States. |bNational Aeronautics and Space Administration. |=^A5437
830  0 NASA technical memorandum |v208896. |=^A467613
949    NAS 1.15:208896 |wsudoc |hjoyner32 |ojjlm
596    1
998    4474332