Numerical simulation of supersonic flow using a new analytical bleed boundary condition

Title
  1. Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.
Published by
  1. [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Author
  1. Harloff, G. J.

Details

Additional authors
  1. Smith, G. E.
  2. United States. National Aeronautics and Space Administration.
Description
  1. 1 v.
Series statement
  1. NASA contractor report ; 198368
Uniform title
  1. NASA contractor report ; NASA CR-198368.
Subject
  1. Boundary layer control
  2. Computational fluid dynamics
  3. Flow distribution
  4. Oblique shock waves
  5. Shock wave interaction
  6. Supersonic boundary layers
  7. Supersonic flow
  8. Supersonic inlets
Call number
  1. READEX Microfiche NAS 1.26:198368
Note
  1. Distributed to depository libraries in microfiche.
  2. Shipping list no.: 96-0232-M.
Reproduction (note)
  1. Microfiche.
Author
  1. Harloff, G. J.
Title
  1. Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.
Imprint
  1. [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
  1. NASA contractor report ; 198368
  2. NASA contractor report ; NASA CR-198368.
Reproduction
  1. Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added author
  1. Smith, G. E.
  2. United States. National Aeronautics and Space Administration.
Gpo item no.
  1. 0830-H-14 (MF)
Sudoc no.
  1. NAS 1.26:198368
Research call number
  1. READEX Microfiche NAS 1.26:198368
View in legacy catalog