Hayes - Hypersonic Inviscid Flow

In the references cited we have used, as far as possible, the abbreviations for journals and reports used by Applied Mechanics Reviews. A list of these abbreviations may be found through any recent index number of Applied Mechanics Reviews.

Transliteration of Russian names has essentially followed the system adopted by the Library of Congress, but with no distinction between e and e or between and , and with yu used for and ya for . Russian titles have been translated into English, but where a translation is indicated the title given is that appearing on the translated version. A source of an English translation for all cited Russian references has been given whenever known to the authors. Translations listed as M. D. Friedman Transl . may be obtained from the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia. The sources of all other translations are self-explanatory.

Except where a distinguishing reference to a superseded more informal report was desired, we have consistently referenced the final published version of a paper if available.

Anderson, W. A.

See Xerikos and Anderson.

Antonov, A. M., and Hayes, W. D.

• [1] Calculation of the hypersonic flow about blunt bodies, J. Appl. Math. Mech. ( Prikl. Mat. Mekh., pp. 347-352) , no. 2 (1966), to appear.

Appleton, J. P.

• [1] Structure of a Prandtl-Meyer expansion in an ideal dissociating gas, Physics of Fluids , 1057-1062 (1963).
• [2] Aerodynamic pitching derivatives of a wedge in hypersonic flow, AIAA J. , 2034-2036 (1964).

ARO

• [1] Mollier diagram for equilibrium air, ARO, Inc., Arnold Air Force Station, Tenn., 1964.

Ashley, H.

See Zartarian, Hsu, and Ashley.

Ashley, H., and Zartarian, G.

• [1] Piston theorya new aerodynamic tool for the aeroelastician, J. Aero. Sci. , 11091118 (1956).

Babaev, D. A.

• [1] Numerical solution of the problem of flow round the upper surface of a triangular wing by a supersonic stream, Zh. Vychislitelnoi Mat. i Mat. Fiz. , 278-289 (1962). Transl. in U.S.S.R. Comput. Math. and Math. Phys., 296308.
• [2] The numerical solution of the problem of the flow about the lower surface of a triangular wing in a supersonic stream, Zh. Vychislitelnoi Mat. i Mat. Fiz. , 10861101 (1962). Transl. in U.S.S.R. Comput. Math. and Math. Phys., 13051324. Also AIAA J. , 22242231 (1963).
• [3] Flow about a triangular wing for large values of M, Zh. Vychislitelnoi Mat. i Mat. Fiz. , 397-400 (1963). Transl. in U.S.S.R. Comput. Math. and Math. Phys., 528532.

Babenko, K. I., Voskresenskii, G. P., Lyubimov, A. N., and Rusanov, V. V.

• [1] Three Dimensional Flows of an Ideal Gas Past Smooth Bodies. Izdat. Nauka, Moscow, 1964.

Bam-Zelikovich, G. M., Bunimovich, A. I., and Mikhailova, M. P.

• [1] The motion of slender bodies at hypersonic speeds, Collection of Papers No. , Teoretich. Gidromekhanika. Oborongiz, Moscow, 1949. See also Izv. Akad. Nauk SSSR, Otd. Tekhn. Nauk, Mekh. i Mashinostr., 1959, no. 1, 34-40.

Baron, J. R.

See Shih and Baron.

Bartos, J.

See Gerber and Bartos.

Batchelder, R. A.

• [1] An inverse method for inviscid ideal gas flow fields behind analytic shock shapes, Rep. SM-42588, Santa Monica Div., Douglas Aircraft Co., Inc., Santa Monica, Calif., 1963.

Bates, D. R. (ed.)

• [1] Atomic and Molecular Processes. Academic Press, New York, 1962.

Bausch, H.

• [1] Die Singularittsstelle in der Grenzschichtmethode der Hyperschallgasdynamik, ZAMM , 557-564 (1962). See also Vestnik Leningrad. Univ. 1963, no. 1, 8689.

Bazzhin, A. P.

• [1] On the calculation of hypersonic gas flow past a flat plate with a detached shock wave, Inzhen. Zh., Moscow , 222227 (1963).

Bazzhin, A. P., and Gladkov, A. A.

• [1] On a solution of the inverse problem by the method of series expansion, Inzhen. Zh., Moscow , 517-518 (1963).

Bechert, K.

• [1] ber die Differentialgleichungen der Wellenausbreitungen in Gasen, Ann. Physik , 357372 (1941).

Bedder, D.

See Freeman, Cash, and Bedder.

Belotserkovskii, O. M.

• [1] Flow past a circular cylinder with a detached shock, Dokladi Akad. Nauk SSSR , 509512 (1957). M. D. Friedman Transl. no. B-131.
• [2] Flow with a detached shock wave about a symmetrical profile, J. Appl. Math. Mech. ( Prikl . Mat. Mekh. ) , 279-296 (1958).
• [3] Flow past a circular cylinder with a detached shock wave, Vychislitelnoi Mat., 1958, no. 3, 149-185. Transl. as Tech. Memo. no. RAD-9-TM-59-66, Research and Advanced Dev. Div., Avco Corp., Wilmington, Mass., 1959.
• [4] The Calculation of Flows Past Axisymmetric Bodies with Detached Shock Waves ( Calculation Formulas and Flow Field Tables ). Vychislitelnyi Tsentr Akad. Nauk SSSR, Moscow, 1961. Transl. as Tech. Memo. no. RAD-TM-62-64, Research and Advanced Dev. Div., Avco Corp., Wilmington, Mass., 1962. See also J. Appl. Math. Mech. ( Prikl . Mat. Mekh .) , 744755 (1960).
• [5] Symmetric flow about blunt bodies in a supersonic stream of a perfect and real gas, Zh. Vychisliteloi Mat. i Mat. Fiz. , 10621085 (1962). Transl. in U.S.S.R. Comput. Math. and Math. Phys., 12721304.

Belotserkovskii, O. M., and Chushkin, P. I.

• [1] Supersonic flow past blunt bodies, Arch. Mech. Stos. , 461490 (1962).
• [2] The numerical solution of problems in gas dynamics, Basic Developments in Fluid Dynamics, Vol. I (M. Holt, ed.), pp. 1126. Academic Press, New York, 1965.

Belotserkovskii, O. M., and Dushin, V. K.

• [1] The supersonic flow round blunt bodies of an unbalanced (nonequilibrium) gas stream, Zh. Vychisliteloi Mat. i Mat. Fiz. , 6177 (1964). Transl. in U.S.S.R. Comput. Math. and Math. Phys., 83104.

Berger, S. A.

• [1] Hypersonic flow over cones, Rep. no. 523, Dept. of Aero. Eng., Princeton Univ., Princeton, N. J., 1960.

Bird, G. A.

• [1] Effect of wave interactions on pressure distributions in supersonic and hypersonic flow, AIAA J. , 634639 (1963).

Bird, R. B.

See Hirschfelder, Curtiss, and Bird.

Bloor, M. I. G.

• [1] Determination of the sonic line in hypersonic flow past a blunt body, J. Fluid Mech. , 495501 (1965).

Blythe, P. A.

• [1] The effects of vibrational relaxation on hypersonic flow past blunt bodies, Aeronaut. Quart. , 357373 (1963).

Bogacheva, A. A., and Ladyzhenskii, M. D.

• [1] Hypersonic flow past slender blunted elliptic cones, Inzhen. Zh., Moscow , no. 3, 1420 (1962).

Bogdonoff, S. M.

See Vas, Bogdonoff, and Hammitt.

Bohachevsky, I. O., Rubin, E. L., and Mates, R. E.

• [1] A direct method for computation of nonequilibrium flows with detached shock waves. I: Two-dimensional flows (Bohachevsky and Rubin), AIAA J. J. 4, 600-607 (1966); II: Axisymmetric blunt-body at an angle of attack (Bohachevsky and Mates), AIAA J . 4, 776782 (1966).

Bowen, E. N.

See Ivey, Klunker, and Bowen.

Brainerd, J. J.

See Cole and Brainerd.