Dynamic Stability of Blunt Atmospheric Entry Configurations von Winchenbach, Gerald L, Chapman, Gary T, Hathaway, Wayne H, Ramsey, Alvin, Berner, Claude

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Roll motion of a wraparound fin configuration at subsonic and transonic Mach numbers von KIM, Y. H, WINCHENBACH, G. L

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Subsonic and transonic aerodynamics of a wraparound fin configuration von WINCHENBACH, G. L, BUFF, RANDY S, WHYTE, ROBERT H, HATHAWAY, WAYNE H

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Free-flight and wind-tunnel data for a generic fighter configuration von Winchenbach, G.L, Uselton, R. L, Hathaway, W. H, Chelekis, R. M

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Comparison of various drag coefficient expansions using polynomials and splines von Sabot, Sally M, Winchenbach, G.L, Chapman, G.T

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Dynamic stability of blunt atmospheric entry configurations von Winchenbach, G L, Chapman, G T, Hathaway, W H, Ramsey, A, Berner, C

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Aerodynamic Testing in a Free-Flight Spark Range von Winchenbach, G. L

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Aerodynamic testing in a free-flight spark range / G. L. Winchenbach von Winchenbach, G. L

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Free Flight Range Tests of a High Density Armor Piercing Flechette Utilizing Yaw cards von Mayer, Paul C, Winchenbach, G. L

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Free-Flight Investigation of Ablation Effects on the Stability of Conical Reentry Configurations von Welsh, C J, Winchenbach, G L

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Free-Flight Range Tests of Blunted 4-, 4.5- and 5-Caliber Bodies of Revolution with Secant-Ogive, Tangent-Ogive, and Conical Nose Shapes von Watt, R M, Winchenbach, G L

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Description and Capabilities of the Aeroballistic Research Facility von Kittyle,Robert L, Packard,James D, Winchenbach,G L

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Comparison of Various Drag Coefficient Expansions Using Polynomials and Splines von Sabot,S M, Chapman,G T, Winchenbach,G L

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Subsonic Free-Flight Data for a Complex Asymmetric Missile von Whyte, Robert H, Winchenbach, Gerald L, Hathaway, Wayne H

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An Electronic Imaging System for the Aeroballistic Research Facility von Winchenbach, G L, Snyder, D B, Valentino, M A, Macke, H C, Rowe, W J

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Free-flight investigation of the aerodynamic characteristics of a cone at high Mach numbers von WELSH, C. J., WINCHENBACH, G. L., MADAGAN, A. N.

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FREE-FLIGHT INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A 10-DEG SEMIANGLE CONE AT MACH NUMBERS FROM 6 TO 16 von Welsh, C J, Winchenbach, G L, Madagan, A N

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FREE-FLIGHT RANGE TESTS OF THE 20-MM M56A2 SHELL WITH THE M505E3 FUZE von Winchenbach, G L, Watt, R M, Welsh, C J

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Aerodynamic Test and Analysis of a Slender Generic Missile Configuration von Gates, Roger S, Winchenbach, G L, Cipolla, John R, Fische, Mark A

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Description and Capabilities of the aeroballistic Research Facility von Winchenbach,G L, Galanos,D G, Kleist,Judith Sullivan, Lucas,Billy F

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