Page 295 - 48Fundamentals of Compressible Fluid Mechanics
P. 295

14.8. COMBINATION OF THE OBLIQUE SHOCK AND ISENTROPIC EXPANSION257

                                                             for which the following
         table can be obtain (Potto-GDC)         S  - U  W   T
         With the angle of attack the region 3 will at *



                   O
                             *
                                                 S
                                                           T
                                       P
                                                            Q
                          UU
                                                                  J
                                                  Q  I    K
         On the other side the oblique shock (assuming weak shock) results in  I




                   K K U

                                                        c      PRQ  PRQ   K K J U
                                       P Q    K



                           O
                                  O
                   O
                                                                     U
                        K  U J
                                         II
         And the additional information by clicking on the minimal button provides





                                         c       P      S   S  U  PRQ  PRQ    U

                          O
                   O
                                                    P    U K K J U
         The pressure ratio at point 3 is            J


                        U J

                        . .  .



         The pressure ratio at point 4         K     U  -%    J  I  -






                              .
                                                 J








                                         .



                                                                        J





                                               .












                                                                     -







                                        J  I   K

                                                      J



                  .
                              .
         This shows that on expense of small drag large lift can be obtained. Question of



                                                          J  I





         optimum design what is left for the next versions.

               "
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