Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /
by Robert F. Peck.

APA Citation

Peck, R. F., Langley Aeronautical Laboratory., United States. National Advisory Committee for Aeronautics. (1955). Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8. Washington, D.C.: National Advisory Committee for Aeronautics.

MLA Citation

Peck, Robert F, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics. Jet Effects On Longitudinal Trim of an Airplane Configuration Measured At Mach Numbers Between 1.2 And 1.8. Washington, D.C.: National Advisory Committee for Aeronautics, 1955.