Supersonic flow computations for an ASTOVL aircraft configuration
An edition of Supersonic flow computations for an ASTOVL aircraft configuration (1990)
phase 2, part 2
By Sekaripuram Ramakrishnan
Publish Date
1990
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Language
eng
Pages
40
1-2 of 2 Editions
Supersonic flow computations for an ASTOVL aircraft configuration
Pages: 40
Published In: 1990
Publisher: Langley Research Center
Supersonic flow computations for an ASTOVL aircraft configuration
Language: eng
Published In: 1990
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch