H. L. Chevalier

MEASUREMENT OF THE PRESSURE FLUCTUATIONS IN THE TEST SECTION OF THE 16-FOOT TRANSONIC CIRCUIT IN THE FREQUENCY RANGE FROM 5 TO 1000 CPS

H. L. Chevalier, H. E. Todd, 1961 .

An analytical method for predicting the stability and control characteristics of large elastic airplanes at subsonic and supersonic speeds. Part 1 - Analysis. Part 2 - Application

A. R. Dusto, H. L. Chevalier, G. M. Dornfield, 1970 .

Wind loads on solar collector structure

H. L. Chevalier, R. A. Wilke, 1981 .

SOME THEORETICAL CONSIDERATIONS OF A STALL PROOF AIRPLANE

H. L. Chevalier, 1979 .

Summary of theoretical considerations and wind tunnel tests of an aerodynamic spoiler for stall proofing a general aviation airplane

H. L. Chevalier, 1982 .

PRESSURE FLUCTUATIONS RESULTING FROM AN ALTERNATING FLOW SEPARATION AND ATTACHMENT AT TRANSONIC SPEEDS

H. L. Chevalier, J. E. Robertson, 1963 .