Aircraft of the Chaco War 1928-1935 by Antonio L. Sapienza

By Antonio L. Sapienza

Greater than a hundred and fifty by no means earlier than released illustrations, complimented through an exhaustively researched textual content, record the little-known air warfare among Bolivia and Paraguay through the past due Nineteen Twenties and early Nineteen Thirties. complete info of such plane as Fiat C.R. 20s, Curtiss Hawk IIs, Curtiss Ospreys, Potez 25s and all different kinds hired via either fighters, together with acquisition, operations, and markings make this a needs to for historians, modelers, and an individual attracted to golden-age aviation.

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Aircraft of the Chaco War 1928-1935

Greater than a hundred and fifty by no means earlier than released illustrations, complimented via an exhaustively researched textual content, record the little-known air struggle among Bolivia and Paraguay through the overdue Twenties and early Nineteen Thirties. complete info of such plane as Fiat C. R. 20s, Curtiss Hawk IIs, Curtiss Ospreys, Potez 25s and all different forms hired via either fighters, together with acquisition, operations, and markings make this a needs to for historians, modelers, and an individual drawn to golden-age aviation.

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0 0 W W 0 LL Cl 0 ::E a:: 0 LL ell 0- ~ I- Q... Z ...... 0 -Cl LIJ a... ::J 0 3: (f) Ii) C\J I- :::t: ::::l 0.. z LIJ Ii) a:: 0 ::::l .... ) LL Ii) tO c:J 0 Ii) ...... 0 ...... Ii) 0 0 ..... J Ii) 0 ..... 479 FIGURE 2. 479 FIGURE 3. 189 FIGURE 4. 189 FIGURE 5. 831 FIGURE 6. 000 FIGURE 7. 110 PATHS OF INTEGRATION FOR SYMMETRIC AIRFOIL 54 B. Figures 8-13 The input speed distribution for the compressor cascade shown in Figures 8 and 9 was taken from an example prepared, using an earlier version of the design code [23], for Pratt and Whitney Aircraft and tested by the DFVLR in Germany (see also Figure 31).

32. , "Geometry of the complex characteristics in transonic flow," Comm. Pure Appl. , Vol. 21, 1968, pp. 175-185. 33. Whitcomb, R. , "Review of NASA supercritica1 airfoils," Ninth International Congress on Aeronautical Sciences, Haifa, 1974. VI. 1. USERS MANUAL FOR THE DESIGN CODE Introduction This chapter is intended for users of the new design program. is essentially independent of the material discussed earlier. It After studying it readers should be able to run the program effectively. The code, written in Fortran IV, has been run on the CDC 6600 at the Courant Institute to design isolated airfoils and compressor and turbine cascades.

VARIABLE NAMED WAS NOT FOUND 18. vlT DID NOT CONVERGE, HT = 19. NEWTON ITERATION FOR SONIC POINT DID NOT CONVERGE WELL 7. Glossary of TAPE7 Parameters All TAPE7 input parameters are listed below with the proper name, default value, definition, and usage. The order corresponds to the frequency of use in the examples we ran. written DEFAULT VALUE RECOMMENDED. In certain cases we have The user is strongly advised to use the default values for those parameters, especially if there is any difficulty.

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