Wind tunnel tests of thin airfoils oscillating near stall.

"January 1969."

NACA conference on some problems of aircraft operation; a compilation of the papers presented.

"Papers presented ... on October 9 and 10, 1950."

Demand bibliography : computational fluid dynamics /

"Sample."

Basic studies of rotating stall and an investigation of flow-instability sensing devices

pt. 1. Basic studies of rotating stall flow mechanisms.--pt. 2. Investigation of flow-instability sensing devices.

Hypersonic dynamic stability.

pt. 1. Summary [by] L. A. Marshall.--pt. 2. Conical body experimental program [by] R. B. Hobbs, Jr.--pt. 3. Unsteady flow field program [by] H. Rie, E. A. Linkiewicz [and] F. D. Bosworth.

Thermal effects on static aeroelastic stability and control.

v. 1. Methods of predicting structural temperatures due to aerodynamic heating, by A. H. Blessing.--v. 2. Aerodynamics, by J. R Batt.--v. 3. Experimental and analytical methods for the determination of thermally-affected wing deflectional behavior, by R. H. Gallagher.--v. 3. sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn.

Hypersonic free flight research.

pt. 1 Instrumentation evaluation and data analysis, by R. W. Bogle and R. J. Magnus.--pt. 2 Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf.

Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.

"Volumes I through VIII are unclassified while volume IX is classified secret."

Collected works of K. E. Tsiolkovskiy. /

Includes bibliographical references.

General aviation pilot stall awareness training study /

Mode of access: Internet.

Airplane design; a textbook of airplane layout and stress analysis calculations with examples and problems.

"Complementary to ... ʻTechnical aerodynamics' by the same author."--Pref.

La mécanique de l'aviation;

At head of title: R. Devillers ...

Hypersonic gas dynamic charts for equilibrium air /

Errata sheet inserted.

Approximate solutions for nonequilibrium airflow in hypersonic nozzles,

Contract no. AF40(600)-804. AEDC TN-60-181. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee. Air Research and Development Command, United States Air Force."

The aerodynamic appraisal of STOL/VTOL configurations,

"Project no. 9-38-01-000, Task 902; Contract no. DA 44-177-TC-439. U. S. Army transportation Research and Development Command, Transportation Corps, Fort Eustis, Virginia."