Volume 1. Performance Flight Testing. Annex 6B. NACA 1135. Equations, Tables, and Charts for Compressible Flow for Supersonic Aerodynamics.

reportActive / Technical Report | Accession Number: ADA320214 | Open PDF

Abstract:

This report, which is a revision and extension of NACA TN 1428, presents a compilation of equations, tables, and charts useful in the analysis of high-speed flow of a compressible fluid. The equations provide relations for continuous one-dimensional flow, normal and oblique shock waves, and Prandtl-Meyer expansions for both perfect and imperfect gases. The tables present useful dimensionless ratios for continuous one-dimensional flow and for normal shock waves as functions of Mach number for air considered as a perfect gas. One series of charts presents the characteristics of the flow of air considered a perfect gas for oblique shock waves and for cones in a supersonic air stream. A second series shows the effects of caloric imperfections on continuous one-dimensional flow and on the flow through normal and oblique shock waves.

Author(s):
No Author(s) Identified
Author Organization(s):
AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA
Supplementary Note:
ADA320201 ADA320202 ADA320203 ADA320204 ADA320205 ADA320206 ADA320207 ADA320208 ADA320209 ADA320210 ADA320211 ADA320212 ADA320213 ADA320215 ADA320216 ADA320217 ADA320218 ADA320219 ADA320220 ADA320221 ADA320222 ADA320223 ADA320224
Pagination:
0073

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Monitor Series:
USAF-TPS
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_5_Command and Control; JCA_5.3_Planning; JCA_1_Force Support
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
*FLIGHT TESTING, *PERFORMANCE(ENGINEERING), *AERODYNAMIC CHARACTERISTICS, *TABLES(DATA), *CHARTS, *EQUATIONS, *SUPERSONIC CHARACTERISTICS, SHOCK WAVES, COMPRESSIBLE FLOW, COURSES(EDUCATION), MACH NUMBER, FLUID FLOW, ONE DIMENSIONAL FLOW, PRANDTL NUMBER, NORMALITY
Field(s)/Group(s):
Aerodynamics, Information Science, Manufacturing and Industrial Engineering and Control of Production Systems, Fluid Mechanics
Report Date:
1991 Jan 01
Creation Date:
1997 Feb 05